Data Release Notes (DRNs) are provided by the NASA TESS mission for original data processings, data reprocessings, and multisector processings for planet searches. This page highlights important information in the data release notes that might affect data from a given sector. Choose a TESS sector from the drop down list to get the most up to date information.
Sector 1 Information
For full data release notes see: DRN1, DRN42 (reprocessing). For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 352.68 | -64.85 | 222.15 |
Camera 1 | 324.57 | -33.17 | 289.92 |
Camera 2 | 338.58 | -55.08 | 299.88 |
Camera 3 | 19.49 | -71.98 | 157.19 |
Camera 4 | 90.0 | -66.56 | 224.19 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
9 | 2018-07-25 - 2018-08-08 | 70444 - 79968 | Every 2.5 days |
10 | 2018-08-09 - 2018-08-22 | 80782 - 90519 | Every 2.5 days |
Sector Notes
Noted Issue | Description |
Scattered light | In Sector 1, the main stray light features to be aware of are: There is an oscillation in the background with a period of 1 day caused by the rotation of the Earth. The Moon gets quite close to the FOV of Camera 1 at the end of the sector. On the last day of observations, the angle between the Moon and the boresight of Camera 1 is <30◦ , which causes a the large spike. |
Mars | Mars was near opposition during Sector 1 and landed in the field-of-view of Camera 1 for ∼2 days at the beginning of observations. Specifically, it is in Camera 1, CCD 4, output channel D, and visual inspection of the FFIs and target pixel files shows an extremely bright object with excess charge spread across the pixels in this output channel. As a consequence, photometry is unreliable in this section of the CCD in the first ∼510 cadences of the sector. See pgs. 7 and 8 of the DRN for more information. |
Timing precision and accuracy | Due to an error in the spacecraft clock kernel, the two-minute cadence durations vary by ∼0.51 msec and the FFI durations vary by ∼7.8 msec. The changes in the durations are discontinuous and occur at reference points used to interpolate the conversion from space- craft time to TJD. However, these errors are well within TESS’s 1 second timing accuracy requirement. |
Reprocessing Information: DRN42
During TESS’s primary mission several updates were made to various instrument models, algorithms, and pipeline parameters. Below we list what was updated and applied when reprocessing sectors 1-13. Please see DRN42 for a more comprehensive explanation of each update.
Update | Description | |
Instrument models updated: | Electronics model Reference Flux, PRF, and Linearity | |
Calibration Pipeline Module updates: | The 1D bias estimate is now split into two components, a time-dependent scalar correction and a static row-dependent correction. The first two overclock rows were also removed. The propagation of the uncertainty from the 2D bias model was changed. It is a static term and no longer applied to pixel data. | |
Pre-Search Data Conditioning Pipeline Module updates: | The parameters to calibrate the PDC goodness metrics were finalized. | |
Transiting Planet Search Pipeline Module updates: | An initial run of TPS is now used to identify problematic epochs that are assigned “deemphasis weights” in a second and final run of TPS. | |
Compute Optimal Aperture Pipeline Module updates: | The photometric apertures for stars with Tmag less than 11 were slightly increased. | |
Photometric Analysis Pipeline Module updates: | The sky background estimate was modified. A scalar offset is now applied that forces the dimmest background-corrected pixels to values near zero, if those pixels were significantly negative. | |
TESS Input Catalog update: | Targets were reprocessed with version 8 of the TIC. The change affected the apertures assigned to individual targets and the calculations for crowding (CROWDSAP) and flux fraction (FLUXFRAC), and as such the physical properties of TCEs derived from stellar parameters. | |
Timestamps update: | Timestamps were updated to account for previous drift errors and electronic effects. All data from Sectors 1–36 are now registered to a consistent time system. | |
New data flags: | All flags are now consistent with those described in DRN30. | |
Threshold Crossing Event issues: | The planet search of the reprocessed light curves produced a different set of TCEs from the original processed data. There is a high degree of overlap, but not every TCE from previous data releases was recovered. To differentiate between the initial release and this reprocessed data a "pipeline instance number" is included in the filenames of the dv-timeseries, dv-reports, ad dv-result xml files. Larger pin numbers indicate later versions of the software were used to produce the data products. The DR number is also included as a keyword in the export product headers (DATA_REL). |
Sector 2 Information
For full data release notes see: DRN2, DRN42 (reprocessing). For a list of TIC IDs with noted issues, see this list
Sector Summary
Sector-2
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 16.56 | -54.02 | 220.43 |
Camera 1 | 352.08 | -23.06 | 294.47 |
Camera 2 | 5.7 | -44.31 | 302.18 |
Camera 3 | 33.36 | -62.19 | 144.76 |
Camera 4 | 90.0 | -66.57 | 196.63 |
Orbit Summary
Pointing | Spacecraft RA, dec | Spacecraft roll (deg) |
---|---|---|
Southern hemisphere | 16.56, -54.02 | 220.43 |
Sector Notes
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
11 | 2018-08-23 - 2018-09-05 | 91186 - 100583 | Every 2.5 days |
12 | 2018-09-07 - 2018-09-20 | 101620 - 110922 | Every 2.5 days |
Noted Issue | Description |
Scattered light | In Sector 2, the main stray light features to be aware of are: The upturns at the end of each orbit are caused by the Earth rising above the sunshade, which reaches a minimum of ∼50 degrees from the center of Camera 1. The Earth’s daily rotation is evident in the background level. The lower level rise in the first orbit of Camera 1 (days 4–9) is caused by the Moon moving within 30 degrees of the camera boresight. |
Reprocessing Information: DRN42
During TESS’s primary mission several updates were made to various instrument models, algorithms, and pipeline parameters. Below we list what was updated and applied when reprocessing sectors 1-13. Please see DRN42 for a more comprehensive explanation of each update.
Update | Description | |
Instrument models updated: | Electronics model Reference Flux, PRF, and Linearity | |
Calibration Pipeline Module updates: | The 1D bias estimate is now split into two components, a time-dependent scalar correction and a static row-dependent correction. The first two overclock rows were also removed. The propagation of the uncertainty from the 2D bias model was changed. It is a static term and no longer applied to pixel data. | |
Pre-Search Data Conditioning Pipeline Module updates: | The parameters to calibrate the PDC goodness metrics were finalized. | |
Transiting Planet Search Pipeline Module updates: | An initial run of TPS is now used to identify problematic epochs that are assigned “deemphasis weights” in a second and final run of TPS. | |
Compute Optimal Aperture Pipeline Module updates: | The photometric apertures for stars with Tmag less than 11 were slightly increased. | |
Photometric Analysis Pipeline Module updates: | The sky background estimate was modified. A scalar offset is now applied that forces the dimmest background-corrected pixels to values near zero, if those pixels were significantly negative. | |
TESS Input Catalog update: | Targets were reprocessed with version 8 of the TIC. The change affected the apertures assigned to individual targets and the calculations for crowding (CROWDSAP) and flux fraction (FLUXFRAC), and as such the physical properties of TCEs derived from stellar parameters. | |
Timestamps update: | Timestamps were updated to account for previous drift errors and electronic effects. All data from Sectors 1–36 are now registered to a consistent time system. | |
New data flags: | All flags are now consistent with those described in DRN30. | |
Threshold Crossing Event issues: | The planet search of the reprocessed light curves produced a different set of TCEs from the original processed data. There is a high degree of overlap, but not every TCE from previous data releases was recovered. To differentiate between the initial release and this reprocessed data a "pipeline instance number" is included in the filenames of the dv-timeseries, dv-reports, ad dv-result xml files. Larger pin numbers indicate later versions of the software were used to produce the data products. The DR number is also included as a keyword in the export product headers (DATA_REL). |
Sector 3 Information
For full data release notes see: DRN4, DRN42 (reprocessing). For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 36.31 | -44.26 | 213.04 |
Camera 1 | 17.17 | -12.22 | 293.55 |
Camera 2 | 28.46 | -33.91 | 298.06 |
Camera 3 | 47.39 | -53.85 | 131.45 |
Camera 4 | 90.0 | -66.57 | 169.06 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
13 | 2018-09-20 - 2018-10-03 | 111297 - 120978 | Every 2.5 days |
14 | 2018-10-05 - 2018-10-17 | 121788 - 130988 | Every 2.5 days |
Sector Notes
Noted Issue | Description |
Spacecraft Pointing | During sector 3 there were several experiments conducted on the attitude control system (ACS) to improve pointing stability. Tests were conducted during the perigee passages after orbits 12, 13 and 14, as well as the first 3 days of orbit 13 and the last 3 days of orbit 14. During these times, the ACS feedback loop was altered and the calibration parameters tuned. The jitter profile during these times differs substantially from the normal data collection mode, which used the same ACS configuration as in Sectors 1 and 2. Imaging and light curve data during these tests is provided for completeness, but has limited use for scientific applications. Valid data in the standard ACS configuration were collected between TJD 1385.8966 and 1395.4800 in orbit 13 and between TJD 1396.6050 and 1406.2925 in orbit 14, spanning ∼20.4 days of useful observations. |
Scattered Light | In Sector 3, the main stray light feature is caused by the Earth rising above the sunshade near the end of each orbit, resulting in an enhancement of the stray light over parts of each camera’s FOV. |
Timing precision and accuracy | The clock kernel used to process Sector 3 data has a slight error, resulting from extrapolation of timing measurements made during Sector 1. The reported TJD values in all data products are therefore offset by ∼1.2 seconds at the end of orbit 14 (2018-10-17 UTC). |
Reprocessing Information: DRN42
During TESS’s primary mission several updates were made to various instrument models, algorithms, and pipeline parameters. Below we list what was updated and applied when reprocessing sectors 1-13. Please see DRN42 for a more comprehensive explanation of each update.
Update | Description | |
Instrument models updated: | Electronics model Reference Flux, PRF, and Linearity | |
Calibration Pipeline Module updates: | The 1D bias estimate is now split into two components, a time-dependent scalar correction and a static row-dependent correction. The first two overclock rows were also removed. The propagation of the uncertainty from the 2D bias model was changed. It is a static term and no longer applied to pixel data. | |
Pre-Search Data Conditioning Pipeline Module updates: | The parameters to calibrate the PDC goodness metrics were finalized. | |
Transiting Planet Search Pipeline Module updates: | An initial run of TPS is now used to identify problematic epochs that are assigned “deemphasis weights” in a second and final run of TPS. | |
Compute Optimal Aperture Pipeline Module updates: | The photometric apertures for stars with Tmag less than 11 were slightly increased. | |
Photometric Analysis Pipeline Module updates: | The sky background estimate was modified. A scalar offset is now applied that forces the dimmest background-corrected pixels to values near zero, if those pixels were significantly negative. | |
TESS Input Catalog update: | Targets were reprocessed with version 8 of the TIC. The change affected the apertures assigned to individual targets and the calculations for crowding (CROWDSAP) and flux fraction (FLUXFRAC), and as such the physical properties of TCEs derived from stellar parameters. | |
Timestamps update: | Timestamps were updated to account for previous drift errors and electronic effects. All data from Sectors 1–36 are now registered to a consistent time system. | |
New data flags: | All flags are now consistent with those described in DRN30. | |
Threshold Crossing Event issues: | The planet search of the reprocessed light curves produced a different set of TCEs from the original processed data. There is a high degree of overlap, but not every TCE from previous data releases was recovered. To differentiate between the initial release and this reprocessed data a "pipeline instance number" is included in the filenames of the dv-timeseries, dv-reports, ad dv-result xml files. Larger pin numbers indicate later versions of the software were used to produce the data products. The DR number is also included as a keyword in the export product headers (DATA_REL). |
Sector 4 Information
For full data release notes see: DRN5, DRN42 (reprocessing). For a list of TIC IDs with noted issues, see this list
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 55.01 | -36.64 | 202.83 |
Camera 1 | 41.81 | -2.76 | 288.16 |
Camera 2 | 49.88 | -25.47 | 290.17 |
Camera 3 | 61.87 | -47.52 | 117.45 |
Camera 4 | 90.0 | -66.56 | 141.52 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
15 | 2018-10-19 - 2018-11-01 | 132081 - 141159 | Every 2.5 days |
16 | 2018-11-02 - 2018-11-14 | 141908 - 150764 | Every 2.5 days |
Sector Notes
Noted Issue | Description |
Incorrect guide star table | An incorrect table was into the DHU at the beginning of Sector 4. The spacecraft pointing was offset by ∼4 arc-seconds from where it would have pointed had the correct guide star table been loaded. Thus, once the correct guide star table was loaded (TJD 1413.26), the spacecraft pointing shifted by ∼4 arc-seconds. |
Instrument reset | At TJD 1418.54, an interruption in communications between the instrument and space- craft occurred, resulting in an instrument turn-off until TJD 1421.21. No data or telemetry were collected during this period. After the instrument anomaly the heaters were turned on , increasing the camera temperature by ∼ 20◦ to approximately −67◦ C. Once the camera power was restored, the heaters were turned off and the camera temperatures returned to nominal within three days. The temperature increase caused changes in the camera focal plane scale and mean black levels of individual CCD channels. The mean black levels are calibrated out in the SPOC pipeline. |
Spacecraft pointing | Sector 4 was the first set of science observations with an improved Attitude Control System (ACS) algorithm. The new ACS mode displays significantly lower pointing jitter than the previous configuration. |
Scattered light | In Sector 4, the main stray light feature are caused by the Earth rising above the sunshade at the end of each orbit. The Earth reaches a minimum of 35 degrees from the center of Camera 1, and strong glints appear between TJD 1422.2297 and 1423.5020 (orbit 15) and between TJD 1436.1047 and 1436.8353 (orbit 16). |
Timing precision and accuracy | The clock kernel used to process Sector 4 data has a slight error, resulting from extrapolation of timing measurements made during Sector 1. The reported TJD values in all data products are therefore offset by ∼1.6 seconds at the end of orbit 16 (2018-11-14 UTC). |
Reprocessing Information: DRN42
During TESS’s primary mission several updates were made to various instrument models, algorithms, and pipeline parameters. Below we list what was updated and applied when reprocessing sectors 1-13. Please see DRN42 for a more comprehensive explanation of each update.
Update | Description | |
Instrument models updated: | Electronics model Reference Flux, PRF, and Linearity | |
Calibration Pipeline Module updates: | The 1D bias estimate is now split into two components, a time-dependent scalar correction and a static row-dependent correction. The first two overclock rows were also removed. The propagation of the uncertainty from the 2D bias model was changed. It is a static term and no longer applied to pixel data. | |
Pre-Search Data Conditioning Pipeline Module updates: | The parameters to calibrate the PDC goodness metrics were finalized. | |
Transiting Planet Search Pipeline Module updates: | An initial run of TPS is now used to identify problematic epochs that are assigned “deemphasis weights” in a second and final run of TPS. | |
Compute Optimal Aperture Pipeline Module updates: | The photometric apertures for stars with Tmag less than 11 were slightly increased. | |
Photometric Analysis Pipeline Module updates: | The sky background estimate was modified. A scalar offset is now applied that forces the dimmest background-corrected pixels to values near zero, if those pixels were significantly negative. | |
TESS Input Catalog update: | Targets were reprocessed with version 8 of the TIC. The change affected the apertures assigned to individual targets and the calculations for crowding (CROWDSAP) and flux fraction (FLUXFRAC), and as such the physical properties of TCEs derived from stellar parameters. | |
Timestamps update: | Timestamps were updated to account for previous drift errors and electronic effects. All data from Sectors 1–36 are now registered to a consistent time system. | |
New data flags: | All flags are now consistent with those described in DRN30. | |
Threshold Crossing Event issues: | The planet search of the reprocessed light curves produced a different set of TCEs from the original processed data. There is a high degree of overlap, but not every TCE from previous data releases was recovered. To differentiate between the initial release and this reprocessed data a "pipeline instance number" is included in the filenames of the dv-timeseries, dv-reports, ad dv-result xml files. Larger pin numbers indicate later versions of the software were used to produce the data products. The DR number is also included as a keyword in the export product headers (DATA_REL). |
Sector 5 Information
For full data release notes see: DRN7, DRN42 (reprocessing). For a list of TIC IDs with noted issues, see this list
Update: Starting with Sector 5 processing, the SPOC pipeline 1-D Black correction has been changed to a two-component model from the polynomial fit that had been used prior. The two components include: a time-varying correction and a static row-by- row correction. To learn more about this see pg. 8 and 9 of the DRN.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 73.54 | -31.93 | 191.05 |
Camera 1 | 67.06 | 3.53 | 279.38 |
Camera 2 | 71.11 | -20.13 | 279.98 |
Camera 3 | 76.7 | -43.68 | 103.0 |
Camera 4 | 90.0 | -66.56 | 114.14 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
17 | 2018-11-15 - 2018-11-27 | 151467 - 160375 | Every 3.0 days |
18 | 2018-11-29 - 2018-12-11 | 161347 - 170601 | Every 3.0 days |
Sector Notes
Noted Issue | Description |
Guiding | The use of Camera 1 in attitude control was disabled for the last ∼ 0.5 days of orbit 18 (2018-12-11 UTC, cadence #170269) due to strong scattered light signals, and data taken with Camera 1 during this period were excluded from the pipeline analysis. |
Space craft pointing | At the end of orbit 18, the Earth was < 35◦ from the boresight of Camera 1. At these low angles, the level of scattered light is too high for meaningful guide star centroids to be measured - see Guiding issue above. Disabling Camera 1 guiding near the end of the Sector caused a brief impulse in pointing, which settled out within minutes. |
Scattered light | In Sector 5, the main stray light features are caused by the Earth rising above the sunshade at the end of each orbit, and strong glints appear during these times. The Earth moves quite close to the boresight of Camera 1 at the end of orbit 18. |
TJD Calculation | The clock kernel used to calculate TJD in Sector 5 used ranging data collected only through late August, 2018; as a result, the extrapolation to Sector 5 times is slightly off. The error between true and calculated times grew linearly with time since August 2018, so that the calculated TJD values in all data products are offset from the correct values by ∼1.7 seconds at the end of orbit 18 (2018-12-11 UTC). See pg. 7 of the DRN for more information. |
Reprocessing Information: DRN42
During TESS’s primary mission several updates were made to various instrument models, algorithms, and pipeline parameters. Below we list what was updated and applied when reprocessing sectors 1-13. Please see DRN42 for a more comprehensive explanation of each update.
Update | Description | |
Instrument models updated: | Electronics model Reference Flux, PRF, and Linearity | |
Calibration Pipeline Module updates: | The 1D bias estimate is now split into two components, a time-dependent scalar correction and a static row-dependent correction. The first two overclock rows were also removed. The propagation of the uncertainty from the 2D bias model was changed. It is a static term and no longer applied to pixel data. | |
Pre-Search Data Conditioning Pipeline Module updates: | The parameters to calibrate the PDC goodness metrics were finalized. | |
Transiting Planet Search Pipeline Module updates: | An initial run of TPS is now used to identify problematic epochs that are assigned “deemphasis weights” in a second and final run of TPS. | |
Compute Optimal Aperture Pipeline Module updates: | The photometric apertures for stars with Tmag less than 11 were slightly increased. | |
Photometric Analysis Pipeline Module updates: | The sky background estimate was modified. A scalar offset is now applied that forces the dimmest background-corrected pixels to values near zero, if those pixels were significantly negative. | |
TESS Input Catalog update: | Targets were reprocessed with version 8 of the TIC. The change affected the apertures assigned to individual targets and the calculations for crowding (CROWDSAP) and flux fraction (FLUXFRAC), and as such the physical properties of TCEs derived from stellar parameters. | |
Timestamps update: | Timestamps were updated to account for previous drift errors and electronic effects. All data from Sectors 1–36 are now registered to a consistent time system. | |
New data flags: | All flags are now consistent with those described in DRN30. | |
Threshold Crossing Event issues: | The planet search of the reprocessed light curves produced a different set of TCEs from the original processed data. There is a high degree of overlap, but not every TCE from previous data releases was recovered. To differentiate between the initial release and this reprocessed data a "pipeline instance number" is included in the filenames of the dv-timeseries, dv-reports, ad dv-result xml files. Larger pin numbers indicate later versions of the software were used to produce the data products. The DR number is also included as a keyword in the export product headers (DATA_REL). |
Sector 6 Information
For full data release notes see: DRN8, DRN42 (reprocessing). For a list of TIC IDs with noted issues, see this list
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 92.01 | -30.58 | 178.64 |
Camera 1 | 92.81 | 5.41 | 268.82 |
Camera 2 | 92.31 | -18.59 | 268.76 |
Camera 3 | 91.62 | -42.58 | 88.41 |
Camera 4 | 89.99 | -66.56 | 87.05 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
19 | 2018-12-12 - 2018-12-24 | 171185 - 179687 | Every 3.125 days |
20 | 2018-12-25 - 2019-01-06 | 180468 - 189064 | Every 3.125 days |
Sector Notes
Noted Issue | Description |
Data Collection | The first ∼3 days (start 2018-12-15 UTC) of orbit 19 were used to collect calibration data for measuring the pixel-response function of the cameras under the improved pointing system. |
Scattered light | In Sector 6, the main stray light features are caused by the Earth rising above the sunshade at the end of orbit 19, which continues through the start of orbit 20. |
TJD Calculation | The clock kernel used to calculate TJD in Sector 6 used ranging data collected only through late August, 2018; as a result, the extrapolation to Sector 6 times is slightly off. The error between true and calculated times grew linearly with time since August 2018, so that the calculated TJD values in all data products are offset from the correct values by ∼2.0 seconds at the end of orbit 20 (2019-01-06 UTC). See pg. 7 of the DRN for more information. |
Reprocessing Information: DRN42
During TESS’s primary mission several updates were made to various instrument models, algorithms, and pipeline parameters. Below we list what was updated and applied when reprocessing sectors 1-13. Please see DRN42 for a more comprehensive explanation of each update.
Update | Description | |
Instrument models updated: | Electronics model Reference Flux, PRF, and Linearity | |
Calibration Pipeline Module updates: | The 1D bias estimate is now split into two components, a time-dependent scalar correction and a static row-dependent correction. The first two overclock rows were also removed. The propagation of the uncertainty from the 2D bias model was changed. It is a static term and no longer applied to pixel data. | |
Pre-Search Data Conditioning Pipeline Module updates: | The parameters to calibrate the PDC goodness metrics were finalized. | |
Transiting Planet Search Pipeline Module updates: | An initial run of TPS is now used to identify problematic epochs that are assigned “deemphasis weights” in a second and final run of TPS. | |
Compute Optimal Aperture Pipeline Module updates: | The photometric apertures for stars with Tmag less than 11 were slightly increased. | |
Photometric Analysis Pipeline Module updates: | The sky background estimate was modified. A scalar offset is now applied that forces the dimmest background-corrected pixels to values near zero, if those pixels were significantly negative. | |
TESS Input Catalog update: | Targets were reprocessed with version 8 of the TIC. The change affected the apertures assigned to individual targets and the calculations for crowding (CROWDSAP) and flux fraction (FLUXFRAC), and as such the physical properties of TCEs derived from stellar parameters. | |
Timestamps update: | Timestamps were updated to account for previous drift errors and electronic effects. All data from Sectors 1–36 are now registered to a consistent time system. | |
New data flags: | All flags are now consistent with those described in DRN30. | |
Threshold Crossing Event issues: | The planet search of the reprocessed light curves produced a different set of TCEs from the original processed data. There is a high degree of overlap, but not every TCE from previous data releases was recovered. To differentiate between the initial release and this reprocessed data a "pipeline instance number" is included in the filenames of the dv-timeseries, dv-reports, ad dv-result xml files. Larger pin numbers indicate later versions of the software were used to produce the data products. The DR number is also included as a keyword in the export product headers (DATA_REL). |
Sector 7 Information
For full data release notes see: DRN9, DRN42 (reprocessing). For a list of TIC IDs with noted issues, see this list
Update: As of Sector 7, the spacecraft clock kernel has been updated. The estimated accuracy of the TJD values in all products associated with this data release is 50 ms.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 110.26 | -32.63 | 166.45 |
Camera 1 | 118.18 | 2.57 | 258.61 |
Camera 2 | 113.25 | -20.93 | 257.8 |
Camera 3 | 106.36 | -44.24 | 74.01 |
Camera 4 | 90.0 | -66.56 | 60.26 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
21 | 2019-01-08 -- 2019-01-19 | 190203 -- 198420 | Every 3.125 days |
22 | 2019-01-21 -- 2019-02-01 | 199615 -- 207814 | Every 3.125 days |
Sector Notes
Noted Issue | Description |
Scattered light | In Sector 7, the main stray light features are caused by the Earth and Moon rising above the sunshade at the end of orbit 21, which continues through the start of orbit 22. |
Black level residuals | Some channels show a small non-zero residual in the mean black level after calibration that is either static (e.g., camera 3, CCD 2, output D) or slowly time varying (e.g., camera 4, CCD 1, all outputs and camera 4, CCD 3, all outputs). The level of these residuals is minor i.e., ∼ 1e-3 ADU/read and the timescale of variation is of order 5–10 days. These residuals are thought to be caused by the jitter of bright stars on the specific CCD slices, and therefore it is a persistent effect in the rest of the sectors. The impact of these residuals on scientific output is likely negligible. However, the Sector 7 data were calibrated using the updated 1-D black method, from which we do not expect such time-varying residuals. |
Reprocessing Information: DRN42
During TESS’s primary mission several updates were made to various instrument models, algorithms, and pipeline parameters. Below we list what was updated and applied when reprocessing sectors 1-13. Please see DRN42 for a more comprehensive explanation of each update.
Update | Description | |
Instrument models updated: | Electronics model Reference Flux, PRF, and Linearity | |
Calibration Pipeline Module updates: | The 1D bias estimate is now split into two components, a time-dependent scalar correction and a static row-dependent correction. The first two overclock rows were also removed. The propagation of the uncertainty from the 2D bias model was changed. It is a static term and no longer applied to pixel data. | |
Pre-Search Data Conditioning Pipeline Module updates: | The parameters to calibrate the PDC goodness metrics were finalized. | |
Transiting Planet Search Pipeline Module updates: | An initial run of TPS is now used to identify problematic epochs that are assigned “deemphasis weights” in a second and final run of TPS. | |
Compute Optimal Aperture Pipeline Module updates: | The photometric apertures for stars with Tmag less than 11 were slightly increased. | |
Photometric Analysis Pipeline Module updates: | The sky background estimate was modified. A scalar offset is now applied that forces the dimmest background-corrected pixels to values near zero, if those pixels were significantly negative. | |
TESS Input Catalog update: | Targets were reprocessed with version 8 of the TIC. The change affected the apertures assigned to individual targets and the calculations for crowding (CROWDSAP) and flux fraction (FLUXFRAC), and as such the physical properties of TCEs derived from stellar parameters. | |
Timestamps update: | Timestamps were updated to account for previous drift errors and electronic effects. All data from Sectors 1–36 are now registered to a consistent time system. | |
New data flags: | All flags are now consistent with those described in DRN30. | |
Threshold Crossing Event issues: | The planet search of the reprocessed light curves produced a different set of TCEs from the original processed data. There is a high degree of overlap, but not every TCE from previous data releases was recovered. To differentiate between the initial release and this reprocessed data a "pipeline instance number" is included in the filenames of the dv-timeseries, dv-reports, ad dv-result xml files. Larger pin numbers indicate later versions of the software were used to produce the data products. The DR number is also included as a keyword in the export product headers (DATA_REL). |
Sector 8 Information
For full data release notes see: DRN10, DRN42 (reprocessing). For a list of TIC IDs with noted issues, see this list.
Update: The algorithm in the CAL module that removes the 1D bias from raw pixel data was changed. The 1D bias estimate is now split into two components, a time-dependent scalar correction and a static row-dependent correction.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 128.12 | -37.74 | 155.31 |
Camera 1 | 142.37 | -4.18 | 250.66 |
Camera 2 | 133.69 | -26.7 | 248.3 |
Camera 3 | 120.6 | -48.42 | 60.15 |
Camera 4 | 90.0 | -66.56 | 33.85 |
Orbit Summary
Pointing | Spacecraft RA, dec | Spacecraft roll (deg) |
---|---|---|
Southern hemisphere | 128.12, -37.74 | 155.31 |
Sector Notes
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
23 | 2019-02-02 - 2019-02-14 | 208718 - 217159 | Every 3.125 days |
24 | 2019-02-15 - 2019-02-27 | 218018 - 226472 | Every 3.125 days |
Noted Issue | Description |
Instrument reset | At TJD 1531.74, an interruption in communications between the instrument and spacecraft occurred, resulting in an instrument turn-off until TJD 1535.00. No data or telemetry were collected during this period. After the instrument anomaly the heaters were turned on, increasing the camera temperature by ∼ 20◦ to approximately −67◦ C. Once the camera power was restored, the heaters were turned off and the camera temperatures returned to nominal within three days. The temperature increase caused changes in the camera focal plane scale and mean black levels of individual CCD channels. The mean black levels are calibrated out in the SPOC pipeline. Changes in focal plane temperature cause changes in the raw photometry, but the PDC systematic error-correction algorithm removes this effect for most targets. |
Guiding |
The use of Camera 1 in attitude control was disabled at the start of both orbits due to strong scattered light signals. Camera 1 guiding was enabled in orbit 23 on 2019-02-02 UTC (Cadence # 208757), and orbit 24 on 2019-02-15 UTC (Cadence # 218154) |
Space Craft Pointing | At the start of each orbit, the Earth was close to the boresight of Camera 1, and the level of scattered light was too high for meaningful guide star centroids to be measured. Guiding with Camera 1 was therefore disabled at these times. When Camera 1 guiding was re-enabled, the spacecraft attitude shifted by a small amount, about 1 arc-second (0.05 pixels). These times are marked with Attitude Tweak flags in the data products. |
Scattered Light | In Sector 8, the main stray light features are caused by the Earth at the start of each orbit, and the Moon in Camera 1 towards the start of orbit 24.
The algorithm in the CAL module that removes the 1D bias from raw pixel data was changed. The 1D bias estimate is now split into two components, a time-dependent scalar correction and a static row-dependent correction. |
Reprocessing Information: DRN42
During TESS’s primary mission several updates were made to various instrument models, algorithms, and pipeline parameters. Below we list what was updated and applied when reprocessing sectors 1-13. Please see DRN42 for a more comprehensive explanation of each update.
Update | Description | |
Instrument models updated: | Electronics model Reference Flux, PRF, and Linearity | |
Calibration Pipeline Module updates: | The 1D bias estimate is now split into two components, a time-dependent scalar correction and a static row-dependent correction. The first two overclock rows were also removed. The propagation of the uncertainty from the 2D bias model was changed. It is a static term and no longer applied to pixel data. | |
Pre-Search Data Conditioning Pipeline Module updates: | The parameters to calibrate the PDC goodness metrics were finalized. | |
Transiting Planet Search Pipeline Module updates: | An initial run of TPS is now used to identify problematic epochs that are assigned “deemphasis weights” in a second and final run of TPS. | |
Compute Optimal Aperture Pipeline Module updates: | The photometric apertures for stars with Tmag less than 11 were slightly increased. | |
Photometric Analysis Pipeline Module updates: | The sky background estimate was modified. A scalar offset is now applied that forces the dimmest background-corrected pixels to values near zero, if those pixels were significantly negative. | |
TESS Input Catalog update: | Targets were reprocessed with version 8 of the TIC. The change affected the apertures assigned to individual targets and the calculations for crowding (CROWDSAP) and flux fraction (FLUXFRAC), and as such the physical properties of TCEs derived from stellar parameters. | |
Timestamps update: | Timestamps were updated to account for previous drift errors and electronic effects. All data from Sectors 1–36 are now registered to a consistent time system. | |
New data flags: | All flags are now consistent with those described in DRN30. | |
Threshold Crossing Event issues: | The planet search of the reprocessed light curves produced a different set of TCEs from the original processed data. There is a high degree of overlap, but not every TCE from previous data releases was recovered. To differentiate between the initial release and this reprocessed data a "pipeline instance number" is included in the filenames of the dv-timeseries, dv-reports, ad dv-result xml files. Larger pin numbers indicate later versions of the software were used to produce the data products. The DR number is also included as a keyword in the export product headers (DATA_REL). |
Sector 9 Information
For full data release notes see: DRN11, DRN42 (reprocessing). For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 145.91 | -45.3 | 145.92 |
Camera 1 | 165.7 | -13.46 | 246.09 |
Camera 2 | 154.09 | -35.04 | 241.22 |
Camera 3 | 134.27 | -54.73 | 46.95 |
Camera 4 | 90.0 | -66.56 | 7.72 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
25 | 2019-02-28 - 2019-03-13 | 227348 - 236222 | Every 3.125 days |
26 | 2019-03-14 - 2019-03-25 | 237073 - 245534 | Every 3.125 days |
Sector Notes
Noted Issue | Description |
Guiding | The use of Camera 1 in attitude control was disabled at the start of both orbits due to strong scattered light signals. Camera 1 guiding was enabled in orbit 25 on 2019-03-01 UTC (Cadence # 227733), and orbit 28 on 2019-03-14 UTC (Cadence # 237273). |
Space Craft Pointing | At the start of each orbit, the Earth was close to the boresight of Camera 1, and the level of scattered light was too high for meaningful guide star centroids to be measured. Guiding with Camera 1 was therefore disabled at these times, and attitude control was done using only inputs from Camera 4. When Camera 1 guiding was re-enabled, the spacecraft attitude shifted by a small amount, about 1 arc-second (0.05 pixels). |
Scattered Light | In Sector 9, the main stray light features are caused by the Earth at the start of each orbit, and the Moon in Camera 1 in the first five days of orbit 26. |
Reprocessing Information: DRN42
During TESS’s primary mission several updates were made to various instrument models, algorithms, and pipeline parameters. Below we list what was updated and applied when reprocessing sectors 1-13. Please see DRN42 for a more comprehensive explanation of each update.
Update | Description | |
Instrument models updated: | Electronics model Reference Flux, PRF, and Linearity | |
Calibration Pipeline Module updates: | The 1D bias estimate is now split into two components, a time-dependent scalar correction and a static row-dependent correction. The first two overclock rows were also removed. The propagation of the uncertainty from the 2D bias model was changed. It is a static term and no longer applied to pixel data. | |
Pre-Search Data Conditioning Pipeline Module updates: | The parameters to calibrate the PDC goodness metrics were finalized. | |
Transiting Planet Search Pipeline Module updates: | An initial run of TPS is now used to identify problematic epochs that are assigned “deemphasis weights” in a second and final run of TPS. | |
Compute Optimal Aperture Pipeline Module updates: | The photometric apertures for stars with Tmag less than 11 were slightly increased. | |
Photometric Analysis Pipeline Module updates: | The sky background estimate was modified. A scalar offset is now applied that forces the dimmest background-corrected pixels to values near zero, if those pixels were significantly negative. | |
TESS Input Catalog update: | Targets were reprocessed with version 8 of the TIC. The change affected the apertures assigned to individual targets and the calculations for crowding (CROWDSAP) and flux fraction (FLUXFRAC), and as such the physical properties of TCEs derived from stellar parameters. | |
Timestamps update: | Timestamps were updated to account for previous drift errors and electronic effects. All data from Sectors 1–36 are now registered to a consistent time system. | |
New data flags: | All flags are now consistent with those described in DRN30. | |
Threshold Crossing Event issues: | The planet search of the reprocessed light curves produced a different set of TCEs from the original processed data. There is a high degree of overlap, but not every TCE from previous data releases was recovered. To differentiate between the initial release and this reprocessed data a "pipeline instance number" is included in the filenames of the dv-timeseries, dv-reports, ad dv-result xml files. Larger pin numbers indicate later versions of the software were used to produce the data products. The DR number is also included as a keyword in the export product headers (DATA_REL). |
Sector 10 Information
For full data release notes see: DRN14, DRN42 (reprocessing). For a list of TIC IDs with noted issues, see this list.
Update: In sector 10, a new linearity model is used in pixel calibration. The differences between new and old linearity model are quite small over the majority of the dynamic range of the CCDs, rising to ∼ 1 − 2% near pixel saturation. This new linearity model will be applied to all sector data from Sector 10 on, and it will be applied to data from Sectors 1-9 when those data are reprocessed.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 165.05 | -54.82 | 139.17 |
Camera 1 | 189.9 | -23.89 | 245.67 |
Camera 2 | 176.16 | -45.14 | 237.72 |
Camera 3 | 147.7 | -62.89 | 34.26 |
Camera 4 | 90.0 | -66.56 | 341.28 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
27 | 2019-03-26 - 2019-04-08 | 246223 - 255117 | Every 3.125 days |
28 | 2019-04-09 - 2019-04-22 | 255821 - 265122 | Every 3.125 days |
Sector Notes
Noted Issue | Description |
Guiding | The use of Camera 1 in attitude control was disabled at the start of both orbits due to strong scattered light signals. Camera 1 guiding was enabled in orbit 27 on 2019-03-28 UTC (Cadence # 247263), and orbit 28 on 2019-04-11 UTC (Cadence # 257233) |
Spacecraft Pointing | At the start of each orbit, the Earth was close to the boresight of Camera 1, and the level of scattered light was too high for meaningful guide star centroids to be measured. Guiding with Camera 1 was therefore disabled at these times, and attitude control was done using only inputs from Camera 4. When Camera 1 guiding was re-enabled, the spacecraft attitude shifted by a small amount, about 1 arc-second (0.05 pixels). |
Scattered Light | In Sector 10, the main stray light features are caused by the Earth at the start of each orbit. |
Reprocessing Information: DRN42
During TESS’s primary mission several updates were made to various instrument models, algorithms, and pipeline parameters. Below we list what was updated and applied when reprocessing sectors 1-13. Please see DRN42 for a more comprehensive explanation of each update.
Update | Description | |
Instrument models updated: | Electronics model Reference Flux, PRF, and Linearity | |
Calibration Pipeline Module updates: | The 1D bias estimate is now split into two components, a time-dependent scalar correction and a static row-dependent correction. The first two overclock rows were also removed. The propagation of the uncertainty from the 2D bias model was changed. It is a static term and no longer applied to pixel data. | |
Pre-Search Data Conditioning Pipeline Module updates: | The parameters to calibrate the PDC goodness metrics were finalized. | |
Transiting Planet Search Pipeline Module updates: | An initial run of TPS is now used to identify problematic epochs that are assigned “deemphasis weights” in a second and final run of TPS. | |
Compute Optimal Aperture Pipeline Module updates: | The photometric apertures for stars with Tmag less than 11 were slightly increased. | |
Photometric Analysis Pipeline Module updates: | The sky background estimate was modified. A scalar offset is now applied that forces the dimmest background-corrected pixels to values near zero, if those pixels were significantly negative. | |
TESS Input Catalog update: | Targets were reprocessed with version 8 of the TIC. The change affected the apertures assigned to individual targets and the calculations for crowding (CROWDSAP) and flux fraction (FLUXFRAC), and as such the physical properties of TCEs derived from stellar parameters. | |
Timestamps update: | Timestamps were updated to account for previous drift errors and electronic effects. All data from Sectors 1–36 are now registered to a consistent time system. | |
New data flags: | All flags are now consistent with those described in DRN30. | |
Threshold Crossing Event issues: | The planet search of the reprocessed light curves produced a different set of TCEs from the original processed data. There is a high degree of overlap, but not every TCE from previous data releases was recovered. To differentiate between the initial release and this reprocessed data a "pipeline instance number" is included in the filenames of the dv-timeseries, dv-reports, ad dv-result xml files. Larger pin numbers indicate later versions of the software were used to produce the data products. The DR number is also included as a keyword in the export product headers (DATA_REL). |
Sector 11 Information
For full data release notes see: DRN16, DRN42 (reprocessing). For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 189.12 | -65.54 | 138.08 |
Camera 1 | 217.3 | -33.73 | 250.57 |
Camera 2 | 203.4 | -55.72 | 240.58 |
Camera 3 | 161.39 | -72.63 | 22.06 |
Camera 4 | 90.0 | -66.56 | 314.08 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
29 | 2019-04-23 - 2019-05-06 | 265908 - 275212 | Every 3.125 days |
30 | 2019-05-07 - 2019-05-20 | 275991 - 285434 | Every 3.125 days |
Sector Notes
Noted Issue | Description |
Guiding | The use of Camera 1 in attitude control was disabled at the start of both orbits due to strong scattered light signals. Camera 1 guiding was enabled in orbit 29 on 2019-04-26 UTC (Cadence # 268190), and orbit 30 on 2019-05-10 UTC (Cadence # 278455). |
Space Craft Pointing | At the start of each orbit, the Earth was close to the boresight of Camera 1, and the level of scattered light was too high for meaningful guide star centroids to be measured. Guiding with Camera 1 was therefore disabled at these times, and attitude control was done using only inputs from Camera 4. When Camera 1 guiding was re-enabled, the spacecraft attitude shifted by a small amount, about 1 arc-second (0.05 pixels). |
Scattered Light | In Sector 11, the main stray light features are caused by the Earth at the start of each orbit. |
Reprocessing Information: DRN42
During TESS’s primary mission several updates were made to various instrument models, algorithms, and pipeline parameters. Below we list what was updated and applied when reprocessing sectors 1-13. Please see DRN42 for a more comprehensive explanation of each update.
Update | Description | |
Instrument models updated: | Electronics model Reference Flux, PRF, and Linearity | |
Pre-Search Data Conditioning Pipeline Module updates: | The parameters to calibrate the PDC goodness metrics were finalized. | |
Transiting Planet Search Pipeline Module updates: | An initial run of TPS is now used to identify problematic epochs that are assigned “deemphasis weights” in a second and final run of TPS. | |
Compute Optimal Aperture Pipeline Module updates: | The photometric apertures for stars with Tmag less than 11 were slightly increased. | |
Photometric Analysis Pipeline Module updates: | The sky background estimate was modified. A scalar offset is now applied that forces the dimmest background-corrected pixels to values near zero, if those pixels were significantly negative. | |
TESS Input Catalog update: | Targets were reprocessed with version 8 of the TIC. The change affected the apertures assigned to individual targets and the calculations for crowding (CROWDSAP) and flux fraction (FLUXFRAC), and as such the physical properties of TCEs derived from stellar parameters. | |
Timestamps update: | Timestamps were updated to account for previous drift errors and electronic effects. All data from Sectors 1–36 are now registered to a consistent time system. | |
New data flags: | All flags are now consistent with those described in DRN30. | |
Threshold Crossing Event issues: | The planet search of the reprocessed light curves produced a different set of TCEs from the original processed data. There is a high degree of overlap, but not every TCE from previous data releases was recovered. To differentiate between the initial release and this reprocessed data a "pipeline instance number" is included in the filenames of the dv-timeseries, dv-reports, ad dv-result xml files. Larger pin numbers indicate later versions of the software were used to produce the data products. The DR number is also included as a keyword in the export product headers (DATA_REL). |
Sector 12 Information
For full data release notes see: DRN17, DRN42 (reprocessing). For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 229.59 | -75.13 | 153.98 |
Camera 1 | 249.34 | -40.26 | 261.51 |
Camera 2 | 241.52 | -63.82 | 255.21 |
Camera 3 | 177.3 | -83.38 | 12.37 |
Camera 4 | 90.01 | -66.56 | 286.45 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
31 | 2019-05-21 - 2019-06-04 | 286196 - 296309 | Every 3.125 days |
32 | 2019-06-05 - 2019-06-18 | 297056 - 306314 | Every 3.125 days |
Sector Notes
Noted Issue | Description |
Space Craft Pointing | Due to scattered light from the Earth Camera 1 was disabled and Camera 4 alone was used for guiding in all of orbit 31. This configuration causes the apparent pointing of Cameras 1, 2 and 3 to drift by larger amounts than in other sectors due to differential velocity aberration. The amplitude of the drift depends on each camera, and has a maximum value of 3 arc-seconds (0.14 pixels) in Camera 1 from the beginning to end of orbit 31. In orbit 32, both Camera 1 and Camera 4 were used for guiding for the entire duration of the orbit. |
Scattered Light | In Sector 12, the main stray light features are caused by the Earth and Moon at the start of each orbit. |
Reprocessing Information: DRN42
During TESS’s primary mission several updates were made to various instrument models, algorithms, and pipeline parameters. Below we list what was updated and applied when reprocessing sectors 1-13. Please see DRN42 for a more comprehensive explanation of each update.
Update | Description | |
Instrument models updated: | Electronics model Reference Flux, PRF, and Linearity | |
Calibration Pipeline Module updates: | The 1D bias estimate is now split into two components, a time-dependent scalar correction and a static row-dependent correction. The first two overclock rows were also removed. The propagation of the uncertainty from the 2D bias model was changed. It is a static term and no longer applied to pixel data. | |
Pre-Search Data Conditioning Pipeline Module updates: | The parameters to calibrate the PDC goodness metrics were finalized. | |
Transiting Planet Search Pipeline Module updates: | An initial run of TPS is now used to identify problematic epochs that are assigned “deemphasis weights” in a second and final run of TPS. | |
Compute Optimal Aperture Pipeline Module updates: | The photometric apertures for stars with Tmag less than 11 were slightly increased. | |
Photometric Analysis Pipeline Module updates: | The sky background estimate was modified. A scalar offset is now applied that forces the dimmest background-corrected pixels to values near zero, if those pixels were significantly negative. | |
TESS Input Catalog update: | Targets were reprocessed with version 8 of the TIC. The change affected the apertures assigned to individual targets and the calculations for crowding (CROWDSAP) and flux fraction (FLUXFRAC), and as such the physical properties of TCEs derived from stellar parameters. | |
Timestamps update: | Timestamps were updated to account for previous drift errors and electronic effects. All data from Sectors 1–36 are now registered to a consistent time system. | |
New data flags: | All flags are now consistent with those described in DRN30. | |
Threshold Crossing Event issues: | The planet search of the reprocessed light curves produced a different set of TCEs from the original processed data. There is a high degree of overlap, but not every TCE from previous data releases was recovered. To differentiate between the initial release and this reprocessed data a "pipeline instance number" is included in the filenames of the dv-timeseries, dv-reports, ad dv-result xml files. Larger pin numbers indicate later versions of the software were used to produce the data products. The DR number is also included as a keyword in the export product headers (DATA_REL). |
Sector 13 Information
For full data release notes see: DRN18, DRN42 (reprocessing). For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 298.67 | -76.33 | 198.94 |
Camera 1 | 284.05 | -40.9 | 275.82 |
Camera 2 | 289.59 | -64.68 | 280.33 |
Camera 3 | 357.94 | -85.5 | 167.75 |
Camera 4 | 90.01 | -66.56 | 258.88 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
33 | 2019-06-19 - 2019-07-03 | 307051 - 316969 | Every 3.375 days |
34 | 2019-07-04 - 2019-07-17 | 317638 - 327529 | Every 3.375 days |
Sector Notes
Noted Issue | Description |
Star tracker anomaly | There was a single upset in the star trackers on the spacecraft bus. This resulted in a complicated interaction between the instrument quaternions and attitude control system. This interaction caused the spacecraft to fall out of fine pointing for approximately 1.25 hours from TJD 1665.2983 to 1665.350. During this time, the spacecraft exhibited increased pointing jitter - see page 3 of the DRN for more information. |
Spacecraft pointing | Due to the proximity of the Moon to the boresight of Camera 1, guiding with Camera 1 was disabled and Camera 4 alone was used for guiding in all of orbit 33. In Orbit 34, both Camera 1 and Camera 4 were used for guiding for the entire duration of the orbit. |
Scattered light | In Sector 13, the main stray light features are caused by the Moon and Earth in the first three quarters of each orbit. |
Reprocessing Information: DRN42
During TESS’s primary mission several updates were made to various instrument models, algorithms, and pipeline parameters. Below we list what was updated and applied when reprocessing sectors 1-13. Please see DRN42 for a more comprehensive explanation of each update.
Update | Description | |
Instrument models updated: | Electronics model Reference Flux, PRF, and Linearity | |
Calibration Pipeline Module updates: | The 1D bias estimate is now split into two components, a time-dependent scalar correction and a static row-dependent correction. The first two overclock rows were also removed. The propagation of the uncertainty from the 2D bias model was changed. It is a static term and no longer applied to pixel data. | |
Pre-Search Data Conditioning Pipeline Module updates: | The parameters to calibrate the PDC goodness metrics were finalized. | |
Transiting Planet Search Pipeline Module updates: | An initial run of TPS is now used to identify problematic epochs that are assigned “deemphasis weights” in a second and final run of TPS. | |
Compute Optimal Aperture Pipeline Module updates: | The photometric apertures for stars with Tmag less than 11 were slightly increased. | |
Photometric Analysis Pipeline Module updates: | The sky background estimate was modified. A scalar offset is now applied that forces the dimmest background-corrected pixels to values near zero, if those pixels were significantly negative. | |
TESS Input Catalog update: | Targets were reprocessed with version 8 of the TIC. The change affected the apertures assigned to individual targets and the calculations for crowding (CROWDSAP) and flux fraction (FLUXFRAC), and as such the physical properties of TCEs derived from stellar parameters. | |
Timestamps update: | Timestamps were updated to account for previous drift errors and electronic effects. All data from Sectors 1–36 are now registered to a consistent time system. | |
New data flags: | All flags are now consistent with those described in DRN30. | |
Threshold Crossing Event issues: | The planet search of the reprocessed light curves produced a different set of TCEs from the original processed data. There is a high degree of overlap, but not every TCE from previous data releases was recovered. To differentiate between the initial release and this reprocessed data a "pipeline instance number" is included in the filenames of the dv-timeseries, dv-reports, ad dv-result xml files. Larger pin numbers indicate later versions of the software were used to produce the data products. The DR number is also included as a keyword in the export product headers (DATA_REL). |
Sector 14 Information
For full data release notes see: DRN19, DRN30 (reprocessing). For a list of TIC IDs with noted issues, see this list.
Updates:
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 276.72 | 62.48 | 32.23 |
Camera 1 | 297.76 | 29.19 | 106.4 |
Camera 2 | 287.05 | 51.83 | 113.5 |
Camera 3 | 256.18 | 71.57 | 321.23 |
Camera 4 | 174.64 | 71.3 | 39.75 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
35 | 2019-07-18 - 2019-07-31 | 328243 - 337632 | Every 4.4 days |
36 | 2019-08-01 - 2019-08-14 | 338316 - 347579 | Every 4.4 days |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | This is the first sector of the northern ecliptic hemisphere survey. For northern pointings, scattered light from the Earth and Moon is a more persistent issue for Camera 1 and Camera 2 than for southern pointings. For this reason, the spacecraft pointing was set at +85 degrees in ecliptic latitude, so that Camera 2 and Camera 3 straddle the ecliptic pole Camera 1 still suffers from strong scattered light signals, and so guiding was disabled in Camera 1 for both orbits 35 and 36. Camera 4 alone was used for guiding in all of orbits 35 and 36. |
Scattered light | In Sector 14, the Earth is above the sunshade for almost the entire sector, and the backgrounds are somewhat higher for longer periods of time than in other sectors. The 24 hour rotation period of the Earth and several harmonics thereof are also visible as oscillations in the background for most of both orbits. Finally, the Earth passes close to Camera 1 towards the last quarter of each orbit and saturates the detectors—these times were excluded with CCD-specific “Scattered Light” flags. |
Reprocessing Information: DRN30
The data products of sectors 14 to 19 were generated using version 4.0 of the science processing pipeline and conform to the final set of data anomaly flags. A detailed description of the changes in the data products can be found in DRN30, but a summary is provided here.
Update | Description |
Timestamps: | For 2 minute cadence and FFI data the timestamps were made more accurate. The differences between reprocessed data and previous data releases are less than 2.0 seconds in all cases. |
Photometric apertures: | The apertures were increased in size for targets with Tmag less than 11. |
Data Anomaly Flags: | Three new flags were added to mitigate the effects of scattered light; - Cadences with strong scattered light signals or saturation effects that corrupt the calibration data are flagged and removed from analysis. - Scattered light data anomaly flags are customized for each target, and flagged automatically based on the local background level. - Cadences with insufficient targets to derive cotrending basis vectors are flagged and the PDCSAP FLUX light curves are set to NULL at these times The modifications to the data anomaly flags also changed the cotrended light curves produced by PDC. The changes also result in new cotrending basis vectors for each CCD in each sector. The scattered light flags are now only applied to the PDCSAP FLUX light curves. |
Threshold Corssing Event issue: | The planet search of the reprocessed light curves produced a different set of TCEs from the original processed data. Although there is a high degree of overlap between the original and reprocessed data (∼83% of targets produced TCEs in common), new TCEs were produced and not every TCE from previous data releases was recovered. |
Sector 15 Information
For full data release notes see: DRN21, DRN30 (reprocessing). For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 280.4 | 64.07 | 55.43 |
Camera 1 | 316.91 | 35.57 | 116.28 |
Camera 2 | 298.18 | 55.9 | 129.96 |
Camera 3 | 252.38 | 68.63 | 351.2 |
Camera 4 | 196.75 | 60.86 | 42.32 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
37 | 2019-08-15 - 2019-08-28 | 348411 - 357409 | Every 4.25 days |
38 | 2019-08-29 - 2019-09-10 | 358186 - 367167 | Every 4.25 days |
Sector Notes
Noted Issue | Description |
Star tracker anomaly | A single upset event in the star trackers caused the spacecraft to fall out of fine pointing in orbit 38. The issue lasts for 5 minutes at TJD 1725.93651 (cadences 358907, 358908, and 358909). |
Spacecraft pointing | As in Sector 14, the pointing in Sector 15 was set at +85 degrees in ecliptic latitude, so that Camera 2 and Camera 3 straddle the ecliptic pole. Camera 1 still suffers from strong scattered light signals, and so guiding was disabled in Camera 1 for both orbits 37 and 38. Camera 4 alone was used for guiding during this sector. |
Scattered light | In Sector 15, the Earth is above the sunshade for almost the entire sector. The 24 hour rotation period of the Earth and several harmonics thereof are visible as oscillations in the background for most of both orbits. Finally, the Earth passes close to Camera 1 towards the last quarter of each orbit and saturates the detectors—these times were excluded with CCD-specific “Scattered Light” flags. |
Reprocessing Information: DRN30
The data products of sectors 14 to 19 were generated using version 4.0 of the science processing pipeline and conform to the final set of data anomaly flags. A detailed description of the changes in the data products can be found in DRN30, but a summary is provided here.
Update | Description |
Timestamps: | For 2 minute cadence and FFI data the timestamps were made more accurate. The differences between reprocessed data and previous data releases are less than 2.0 seconds in all cases. |
Photometric apertures: | The apertures were increased in size for targets with Tmag less than 11. |
Data Anomaly Flags: | Three new flags were added to mitigate the effects of scattered light; - Cadences with strong scattered light signals or saturation effects that corrupt the calibration data are flagged and removed from analysis. - Scattered light data anomaly flags are customized for each target, and flagged automatically based on the local background level. - Cadences with insufficient targets to derive cotrending basis vectors are flagged and the PDCSAP FLUX light curves are set to NULL at these times The modifications to the data anomaly flags also changed the cotrended light curves produced by PDC. The changes also result in new cotrending basis vectors for each CCD in each sector. The scattered light flags are now only applied to the PDCSAP FLUX light curves. |
Threshold Corssing Event issue: | The planet search of the reprocessed light curves produced a different set of TCEs from the original processed data. Although there is a high degree of overlap between the original and reprocessed data (∼83% of targets produced TCEs in common), new TCEs were produced and not every TCE from previous data releases was recovered. |
Sector 16 Information
For full data release notes see: DRN22, DRN30 (reprocessing). For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 282.44 | 66.14 | 79.47 |
Camera 1 | 336.08 | 44.14 | 123.65 |
Camera 2 | 307.85 | 61.55 | 146.58 |
Camera 3 | 252.91 | 65.5 | 16.51 |
Camera 4 | 214.06 | 51.57 | 50.23 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
39 | 2019-09-12 - 2019-09-23 | 368058 - 376489 | Every 5.83 days |
40 | 2019-09-25 - 2019-10-06 | 377421 - 385822 | Every 5.83 days |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | As in Sector 14 and Sector 15, the pointing in Sector 16 was set at +85 degrees in ecliptic latitude, so that Camera 2 and Camera 3 straddle the ecliptic pole. Both Camera 1 and Camera 4 were used for guiding during this sector. |
Scattered light | In Sector 16, the Earth is above the sunshade for much of the sector, in a similar way as Sector 14 and Sector 15. The 24 hour rotation period of the Earth and several harmonics thereof are visible as oscillations in the background for most of both orbits. |
Reprocessing Information: DRN30
The data products of sectors 14 to 19 were generated using version 4.0 of the science processing pipeline and conform to the final set of data anomaly flags. A detailed description of the changes in the data products can be found in DRN30, but a summary is provided here.
Update | Description |
Timestamps: | For 2 minute cadence and FFI data the timestamps were made more accurate. The differences between reprocessed data and previous data releases are less than 2.0 seconds in all cases. |
Photometric apertures: | The apertures were increased in size for targets with Tmag less than 11. |
Data Anomaly Flags: | Three new flags were added to mitigate the effects of scattered light; - Cadences with strong scattered light signals or saturation effects that corrupt the calibration data are flagged and removed from analysis. - Scattered light data anomaly flags are customized for each target, and flagged automatically based on the local background level. - Cadences with insufficient targets to derive cotrending basis vectors are flagged and the PDCSAP FLUX light curves are set to NULL at these times The modifications to the data anomaly flags also changed the cotrended light curves produced by PDC. The changes also result in new cotrending basis vectors for each CCD in each sector. The scattered light flags are now only applied to the PDCSAP FLUX light curves. |
Threshold Corssing Event issue: | The planet search of the reprocessed light curves produced a different set of TCEs from the original processed data. Although there is a high degree of overlap between the original and reprocessed data (∼83% of targets produced TCEs in common), new TCEs were produced and not every TCE from previous data releases was recovered. |
Sector 17 Information
For full data release notes see: DRN24, DRN30 (reprocessing). For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 351.24 | 57.85 | 41.97 |
Camera 1 | 17.39 | 26.89 | 113.52 |
Camera 2 | 3.29 | 48.23 | 122.3 |
Camera 3 | 331.6 | 65.56 | 329.33 |
Camera 4 | 270.0 | 66.57 | 26.51 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
41 | 2019-10-08 - 2019-10-19 | 386801 - 395164 | Every 3.875 days |
42 | 2019-10-21 - 2019-11-02 | 396193 - 404812 | Every 4.0 days |
Sector Notes
Noted Issue | Description |
Instrument reset | An instrument reset also occurred in orbit 42—no data were collected for six minutes between TJD 1789.18374 and 1789.18790. |
Spacecraft pointing | In Sector 17, the spacecraft pointing returned to the nominal mission pointing with Camera 4 centered on the North Ecliptic Pole. Camera 4 alone was used for guiding in both orbit 41 and orbit 42. |
Scattered light | In Sector 17, the Moon and Earth move into the field of view of Camera 1 towards the end of each orbit. |
Reprocessing Information: DRN30
The data products of sectors 14 to 19 were generated using version 4.0 of the science processing pipeline and conform to the final set of data anomaly flags. A detailed description of the changes in the data products can be found in DRN30, but a summary is provided here.
Update | Description |
Timestamps: | For 2 minute cadence and FFI data the timestamps were made more accurate. The differences between reprocessed data and previous data releases are less than 2.0 seconds in all cases. |
Photometric apertures: | The apertures were increased in size for targets with Tmag less than 11. |
Data Anomaly Flags: | Three new flags were added to mitigate the effects of scattered light; - Cadences with strong scattered light signals or saturation effects that corrupt the calibration data are flagged and removed from analysis. - Scattered light data anomaly flags are customized for each target, and flagged automatically based on the local background level. - Cadences with insufficient targets to derive cotrending basis vectors are flagged and the PDCSAP FLUX light curves are set to NULL at these times The modifications to the data anomaly flags also changed the cotrended light curves produced by PDC. The changes also result in new cotrending basis vectors for each CCD in each sector. The scattered light flags are now only applied to the PDCSAP FLUX light curves. |
Threshold Corssing Event issue: | The planet search of the reprocessed light curves produced a different set of TCEs from the original processed data. Although there is a high degree of overlap between the original and reprocessed data (∼83% of targets produced TCEs in common), new TCEs were produced and not every TCE from previous data releases was recovered. |
Sector 18 Information
For full data release notes see: DRN25, DRN30 (reprocessing). For a list of TIC IDs with noted issues, see this list.
Update:
The FFI timestamps for Sector 18 are incorrect. The readouts of the four cameras are staggered by 0.5 seconds in the following order: Camera 1 (0 second offset), Camera 3 (0.5 second offset), Camera 4 (1.0 second offset), and Camera 2 (1.5 second offset). Although these offsets are correctly incorporated into the timestamps in the target pixel files and light curves, the FFI time stamps are not corrected for the staggered readout. For Sector 1 through Sector 18, the offsets for each camera can be added to the TSTART and TSTOP header values in the FFIs to correct the issue.
In addition, the TSTOP header values in the target pixel files, light curve files, and FFIs are overestimated by 20 ms, and the TIME column of the target pixel files and light curve files are overestimated by 10 ms.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 16.11 | 67.96 | 40.55 |
Camera 1 | 44.14 | 35.61 | 107.46 |
Camera 2 | 30.86 | 57.93 | 117.35 |
Camera 3 | 344.62 | 75.0 | 340.53 |
Camera 4 | 270.0 | 66.56 | 52.16 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
43 | 2019-11-03 - 2019-11-14 | 405501 - 413989 | Every 4.25 days |
44 | 2019-11-15 - 2019-11-27 | 414711 - 423054 | Every 4.5 days |
Sector Notes
Noted Issue | Description |
Instrument shutdown | The spacecraft passed through the shadow of the Earth at the start of orbit 43. During this time, the instrument was turned off and no data were collected for 6.2 hours between TJD 1791.1115 and 1791.3699. The thermal state of the spacecraft changed during this time, and trends in the raw photometry and target positions are apparent after data collection resumed. However, the pipeline effectively removes these trends in the PDC light curves. |
Spacecraft pointing | Camera 4 alone was used for guiding in orbit 43, and both Camera 1 and Camera 4 were used for guiding in orbit 44. |
Scattered light | In Sector 18, the Moon and Earth move close enough to the field of view of Camera 1 at the end of orbit 43 to briefly saturate the detector. |
Reprocessing Information: DRN30
The data products of sectors 14 to 19 were generated using version 4.0 of the science processing pipeline and conform to the final set of data anomaly flags. A detailed description of the changes in the data products can be found in DRN30, but a summary is provided here.
Update | Description |
Timestamps: | For 2 minute cadence and FFI data the timestamps were made more accurate. The differences between reprocessed data and previous data releases are less than 2.0 seconds in all cases. |
Photometric apertures: | The apertures were increased in size for targets with Tmag less than 11. |
Data Anomaly Flags: | Three new flags were added to mitigate the effects of scattered light; - Cadences with strong scattered light signals or saturation effects that corrupt the calibration data are flagged and removed from analysis. - Scattered light data anomaly flags are customized for each target, and flagged automatically based on the local background level. - Cadences with insufficient targets to derive cotrending basis vectors are flagged and the PDCSAP FLUX light curves are set to NULL at these times The modifications to the data anomaly flags also changed the cotrended light curves produced by PDC. The changes also result in new cotrending basis vectors for each CCD in each sector. The scattered light flags are now only applied to the PDCSAP FLUX light curves. |
Threshold Corssing Event issue: | The planet search of the reprocessed light curves produced a different set of TCEs from the original processed data. Although there is a high degree of overlap between the original and reprocessed data (∼83% of targets produced TCEs in common), new TCEs were produced and not every TCE from previous data releases was recovered. |
Sector 19 Information
For full data release notes see: DRN26, DRN30 (reprocessing). For a list of TIC IDs with noted issues, see this list.
Update: The FFI timestamps for Sector 19 do not account for the 0.5 second staggered readouts of the four cameras. The offsets for each camera can be added to the TSTART and TSTOP header values in the FFIs to correct the issue.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 60.2 | 76.23 | 19.65 |
Camera 1 | 75.35 | 40.85 | 96.07 |
Camera 2 | 69.59 | 64.62 | 100.76 |
Camera 3 | 1.54 | 85.31 | 347.82 |
Camera 4 | 270.0 | 66.56 | 78.4 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
45 | 2019-11-28 - 2019-12-10 | 423808 - 432387 | Every 5.0 days |
46 | 2019-12-11 - 2019-12-23 | 433083 - 441859 | Every 5.25 days |
Sector Notes
Noted Issue | Description |
Instrument reset | An instrument reset occurred in orbit 46—no data were collected for four minutes between TJD 1838.73169 and 1838.73586. |
Spacecraft pointing | Camera 1 and Camera 4 were both used for guiding in orbits 45 and 46. |
Scattered light | In Sector 19, there is an increase in the background levels at the end of each orbit due to the Earth, and a smaller affect due to the Moon at the start of orbit 46. |
Reprocessing Information: DRN30
The data products of sectors 14 to 19 were generated using version 4.0 of the science processing pipeline and conform to the final set of data anomaly flags. A detailed description of the changes in the data products can be found in DRN30, but a summary is provided here.
Update | Description |
Timestamps: | For 2 minute cadence and FFI data the timestamps were made more accurate. The differences between reprocessed data and previous data releases are less than 2.0 seconds in all cases. |
Photometric apertures: | The apertures were increased in size for targets with Tmag less than 11. |
Data Anomaly Flags: | Three new flags were added to mitigate the effects of scattered light; - Cadences with strong scattered light signals or saturation effects that corrupt the calibration data are flagged and removed from analysis. - Scattered light data anomaly flags are customized for each target, and flagged automatically based on the local background level. - Cadences with insufficient targets to derive cotrending basis vectors are flagged and the PDCSAP FLUX light curves are set to NULL at these times The modifications to the data anomaly flags also changed the cotrended light curves produced by PDC. The changes also result in new cotrending basis vectors for each CCD in each sector. The scattered light flags are now only applied to the PDCSAP FLUX light curves. |
Threshold Corssing Event issue: | The planet search of the reprocessed light curves produced a different set of TCEs from the original processed data. Although there is a high degree of overlap between the original and reprocessed data (∼83% of targets produced TCEs in common), new TCEs were produced and not every TCE from previous data releases was recovered. |
Sector 20 Information
For full data release notes see: DRN27. For a list of TIC IDs with noted issues, see this list.
Updates:
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 129.39 | 75.25 | 334.57 |
Camera 1 | 110.05 | 40.33 | 81.75 |
Camera 2 | 117.67 | 63.91 | 75.61 |
Camera 3 | 182.33 | 83.58 | 192.29 |
Camera 4 | 270.0 | 66.56 | 105.95 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
47 | 2019-12-24 - 2020-01-06 | 442831 - 451729 | Every 5.35 days |
48 | 2020-01-07 - 2020-01-20 | 452833 - 461784 | Every 5.5 days |
Sector Notes
Noted Issue | Description |
Instrument reset | An instrument reset occurred in orbit 48—no data were collected for two minutes between TJD 1865.49753 and 1865.50030. |
Spacecraft pointing | Camera 1 and Camera 4 were both used for guiding in orbit 47; Camera 4 alone was used for guiding in orbit 48. |
Scattered light | In Sector 20, the Moon passes through the field of view of Camera 1 at the start of orbit 48, saturating the detectors. In Sector 20, new data anomaly flags were added to characterize the different ways that the scattered light can affect the data - see section 2 of the DRN. |
Sector 21 Information
For full data release notes see: DRN29. For a list of TIC IDs with noted issues, see this list.
Update: In Sector 21, the the FFI timestamps have been adjusted for the 0.5 second staggered readouts of the four cameras and the 0.02 second staggered readouts for individual CCDs within a camera. TSTART and TSTOP in the FFIs of previous sectors need to be adjusted for the readout offsets of each camera—see DRN 25 for additional details.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 171.8 | 65.19 | 317.95 |
Camera 1 | 143.64 | 33.45 | 70.32 |
Camera 2 | 157.6 | 55.4 | 60.34 |
Camera 3 | 199.06 | 72.3 | 202.43 |
Camera 4 | 270.0 | 66.56 | 134.95 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
49 | 2020-01-21 - 2020-02-04 | 462941 - 472707 | Every 6.25 days |
50 | 2020-02-05 - 2020-02-18 | 473374 - 482634 | Every 6.5 days |
Sector Notes
Noted Issue | Description |
Instrument reset | Occurred in orbit 50, no data collected for 2 min between TJD 1892.50598 and 1892.50875. |
Spacecraft pointing | Camera 1 and Camera 4 were both used for guiding in orbit 49; Camera 4 alone was used for guiding in orbit 50. |
Scattered light | In Sector 21, the Moon passes through the field of view of Camera 1 at the start of orbit 50, saturating the detectors. A strong glint also appears in Camera 2 during this time. |
Sector 22 Information
For full data release notes see: DRN31. For a list of TIC IDs with noted issues, see this list.
Updates:
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 197.1 | 53.74 | 319.7 |
Camera 1 | 172.75 | 22.78 | 65.49 |
Camera 2 | 186.32 | 44.03 | 57.86 |
Camera 3 | 213.72 | 61.95 | 215.57 |
Camera 4 | 270.0 | 66.56 | 164.08 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
51 | 2020-02-19 - 2020-03-04 | 483729 - 493234 | Every 6.625 days |
52 | 2020-03-05 - 2020-03-17 | 494001 - 503307 | Every 6.75 days |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | Camera 1 and Camera 4 were both used for guiding in orbit 51; Camera 4 alone was used for guiding in orbit 52. |
Scattered light | In Sector 22, the Earth is a significant source of scattered light at the start of both orbits. The Moon also passes through the field of view of Camera 1 at the start of orbit 52, saturating the detectors Camera 4 alone was used for guiding in orbit 52. |
Watchdog resets |
The instrument computer unexpectedly hung, most likely due to space radiation induced errors in the computer processor or memory, resulting in a quick reboot of the computer. There were three watchdog timer resets in Sector 22: on 2/29/20, 3/3/20, and 3/12/20. Besides introducing short gaps in the 2m cadence data, these resets resulted in the loss a total of four FFI cadences. Two 2-minute cadences are missing from TJD 1909.46004 to 1909.4642 (2/29/20), from TJD 1911.9267 to 1911.9309 (3/3/20), and from 1921.0560 to 1921.0602 (3/12/20).
|
Sector 23 Information
For full data release notes see: DRN32. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 217.29 | 43.81 | 327.42 |
Camera 1 | 198.43 | 11.69 | 66.62 |
Camera 2 | 209.58 | 33.41 | 62.26 |
Camera 3 | 228.13 | 53.47 | 229.25 |
Camera 4 | 270.0 | 66.56 | 192.35 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
53 | 2020-03-19 - 2020-04-01 | 504464 - 513659 | 1 |
54 | 2020-04-02 - 2020-04-15 | 514351 - 523742 | 1 |
Sector Notes
Noted Issue | Description |
Instrument issues | The spacecraft passed through the shadow of Earth from approximately TJD 1940.38 – 1940.48. The instrument was not turned off, and other than the instrument heaters turning on resulting in a minor pointing offset, there is no indication that science quality was affected. |
Spacecraft pointing | In orbit 1 of Sector 23, anomalously high pointing jitter was observed for about 1.5 days before the momentum dump starting at ∼ TJD 1936.15. The peak-to-peak amplitude of the jitter is less than 1.5 arcseconds on 2 minute timescales. |
Scattered light | Camera 1 suffered from strong scattered light signals at the beginning of orbit 53 and orbit 54, and so Camera 4 alone was used for guiding during this sector. The Earth is a significant source of scattered light at the start of both orbits. The Moon also passes close to the field of view of Camera 1 during orbit 54. |
Sector 24 Information
For full data release notes see: DRN35. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 261.45 | 63.12 | 317.26 |
Camera 1 | 233.47 | 31.76 | 68.84 |
Camera 2 | 247.74 | 53.46 | 58.98 |
Camera 3 | 286.2 | 70.3 | 204.43 |
Camera 4 | 354.22 | 66.46 | 140.21 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
55 | 2020-04-16 - 2020-04-28 | 524401 - 533442 | 0 |
56 | 2020-04-29 - 2020-05-12 | 534104 - 543474 | 1 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing |
As in Sector 14, the pointing in Sector 24 was set at +85 degrees in ecliptic latitude so that Camera 2 and Camera 3 straddle the ecliptic pole. In Sector 24 there is an anomalously high pointing jitter was observed for the last 3–4 days of that orbit. |
Scattered light | In Sector 24, the Earth is a significant source of scattered light throughout both orbits. |
Sector 25 Information
For full data release notes see: DRN36. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 265.61 | 61.94 | 339.53 |
Camera 1 | 252.26 | 27.06 | 79.35 |
Camera 2 | 259.05 | 50.49 | 75.01 |
Camera 3 | 279.77 | 72.71 | 236.4 |
Camera 4 | 22.74 | 76.64 | 135.42 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
57 | 2020-05-14 - 2020-05-26 | 544444 - 553089 | 1 |
58 | 2020-05-27 - 2020-06-08 | 554009 - 562932 | 1 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing |
As in Sector 14, the pointing in Sector 25 was set at +85 degrees in ecliptic latitude so that Camera 2 and Camera 3 straddled the ecliptic pole. Camera 1 suffered from strong scattered light signals at the beginning of orbit 57 and orbit 58, and so Camera 4 alone was used for guiding during this sector. |
Scattered light | In Sector 25, the Earth is a significant source of scattered light throughout both orbits. |
Sector 26 Information
For full data release notes see: DRN37
For a list of TIC IDs with noted issues, see this list.Update: The TESS spacecraft configuration file was updated from version ‘0187’ to ‘0188’ between orbit 59 and 60. The SPOC data products include this 4 digit identification code near the end of the filename. Therefore the FFIs from orbit 59 have a different 4 digit identification number than those from orbit 60.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 270.14 | 61.56 | 0.6 |
Camera 1 | 270.53 | 25.56 | 90.32 |
Camera 2 | 270.33 | 49.56 | 90.44 |
Camera 3 | 269.69 | 73.56 | 271.02 |
Camera 4 | 92.83 | 82.43 | 87.82 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
59 | 2020-06-09 - 2020-06-21 | 563621 - 572209 | 1 |
60 | 2020-06-22 - 2020-07-04 | 572871 - 581529 | 1 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing |
The pointing in Sector 26 was set at +85 degrees in ecliptic latitude so that Camera 2 and Camera 3 straddle the ecliptic pole. Camera 1 suffered from strong scattered light signals at the midpoint of orbit 59 and orbit 60, and so Camera 4 alone was used for guiding during this sector. |
Scattered light | In Sector 26, the Earth is a significant source of scattered light throughout both orbits. |
- The background correction was updated for the extended mission, with the new method providing improved results for fainter and crowded stars.
- For targets observed in both Year 1 and Year 3, Year 3 processing was done using TIC 8.1 while TIC 7 was used for Year 1 processing; this may result in differences in results for certain targets.
Sector 27 Information
For full data release notes see: DRN38. For a list of TIC IDs with noted issues, see this list.
Updates:
This is the first data release for the extended mission
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 326.85 | -72.43 | 214.51 |
Camera 1 | 301.6 | -38.68 | 282.66 |
Camera 2 | 312.45 | -61.74 | 291.17 |
Camera 3 | 8.6 | -79.81 | 165.21 |
Camera 4 | 90.01 | -66.56 | 244.53 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
61 | 2020-07-05 - 2020-07-17 | 582349 - 590884 | 1 |
62 | 2020-07-18 - 2020-07-30 | 591619 - 599894 | 1 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | Year 3 is a re-observation of the southern ecliptic hemisphere, which will take place over 13 sectors. The pointing strategy is the same as for Year 1, except the locations of Sectors 27–39 are offset in ecliptic longitude with respect to Sectors 1–13. All sectors in Year 3 are planned for a spacecraft pointing of −54 degrees in ecliptic latitude. |
Scattered light | In Sector 27, the Earth is a significant source of scattered light throughout both orbits. |
Sector 28 Information
For full data release notes see: DRN41. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 357.29 | -63.01 | 222.52 |
Camera 1 | 329.49 | -31.62 | 291.12 |
Camera 2 | 343.69 | -53.32 | 300.91 |
Camera 3 | 21.86 | -70.24 | 155.17 |
Camera 4 | 90.0 | -66.56 | 219.52 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
63 | 2020-07-31 - 2020-08-12 | 600761 - 609484 | 1 |
64 | 2020-08-13 - 2020-08-25 | 610341 - 618942 | 1 |
Sector Notes
Noted Issue | Description |
Scattered light | In Sector 28, the Earth introduces scattered light signals at the end of both orbits. |
Sector 29 Information
For full data release notes see: DRN43. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 18.92 | -52.83 | 219.8 |
Camera 1 | 355.01 | -21.83 | 294.62 |
Camera 2 | 8.42 | -43.07 | 301.96 |
Camera 3 | 34.93 | -61.16 | 143.29 |
Camera 4 | 90.0 | -66.57 | 193.5 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
65 | 2020-08-26 - 2020-09-08 | 619761 - 629222 | 1 |
66 | 2020-09-09 - 2020-09-21 | 629904 - 638624 | 1 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | Camera 1 suffered from strong scattered light signals at the end of orbit 65 and orbit 66, and so Camera 4 alone was used for guiding during this sector. |
Scattered light | In Sector 29, the Moon introduces a strong glint in Camera 1 at the end of orbit 65, and the Earth introduces scattered light signals in all cameras at the end of both orbits. |
Sector 30 Information
For full data release notes see: DRN45. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 38.36 | -43.32 | 212.04 |
Camera 1 | 19.83 | -11.1 | 293.17 |
Camera 2 | 30.81 | -32.88 | 297.36 |
Camera 3 | 48.93 | -53.06 | 129.97 |
Camera 4 | 90.0 | -66.57 | 166.08 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
67 | 2020-09-23 - 2020-10-06 | 639666 - 649212 | 1 |
68 | 2020-10-07 - 2020-10-20 | 649979 - 659352 | 1 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | Camera 1 suffered from strong scattered light signals at the end of orbit 67 and orbit 68, and so Camera 4 alone was used for guiding during this sector. |
Scattered light | In Sector 30, the Moon introduces a strong glint in Camera 1 at the end of orbit 67, and the Earth introduces scattered light signals in all cameras at the end of both orbits. |
Sector 31 Information
For full data release notes see: DRN47. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 57.64 | -35.78 | 201.23 |
Camera 1 | 45.34 | -1.64 | 287.09 |
Camera 2 | 52.89 | -24.5 | 288.84 |
Camera 3 | 63.95 | -46.82 | 115.42 |
Camera 4 | 90.0 | -66.56 | 137.62 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
69 | 2020-10-22 - 2020-11-03 | 660279 - 669599 | 1 |
70 | 2020-11-05 - 2020-11-16 | 670609 - 678592 | 1 |
Sector Notes
Noted Issue | Description |
Star tracker anomaly | At UTC 2020-11-16 10:37, there was a star tracker anomaly which led to the instrument being turned off. As a result, the data collection period in orbit 70 ended 2.08 days earlier than scheduled. The cameras were turned on and returned to normal operations on 2020-11-20, at the beginning of Sector 32. |
Spacecraft pointing | Camera 1 suffered from strong scattered light signals at the end of orbit 69 and orbit 70, and so Camera 4 alone was used for guiding during this sector. |
Scattered light | In Sector 31, the Moon introduces a strong glint in Camera 1 at the end of orbit 69, followed by scattered light signals in all cameras caused by the Earth. Due to the star tracker anomaly, no data were taken during periods of high scattered light in orbit 70. |
Sector 32 Information
For full data release notes see:DRN48. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 77.19 | -31.4 | 188.63 |
Camera 1 | 72.12 | 4.28 | 277.38 |
Camera 2 | 75.29 | -19.52 | 277.81 |
Camera 3 | 79.64 | -43.24 | 100.12 |
Camera 4 | 90.0 | -66.56 | 108.78 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
71 | 2020-11-20 - 2020-12-02 | 681670 - 690109 | 1 |
72 | 2020-12-03 - 2020-12-16 | 690829 - 700399 | 1 |
Sector Notes
Noted Issue | Description |
Star tracker anomaly | UTC 2020-11-16 10:37, instrument turned off and collection of data for orbit 71 started 29 hrs later than scheduled. Normal operation started 2020-11-20-17-13-00 UTC. |
Spacecraft pointing | Camera 4 alone was used for guiding in orbit 72. |
Scattered light | In Sector 32, the Moon introduces a strong glint in Camera 1 at the end of orbit 71. |
Sector 33 Information
For full data release notes see: DRN49. For a list of TIC IDs with noted issues, see this list.
Updates:
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 96.6 | -30.78 | 175.54 |
Camera 1 | 99.23 | 5.13 | 266.15 |
Camera 2 | 97.58 | -18.82 | 265.95 |
Camera 3 | 95.34 | -42.74 | 84.78 |
Camera 4 | 90.0 | -66.56 | 80.32 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
73 | 2020-12-18 - 2020-12-30 | 701476 - 710214 | 1 |
74 | 2020-12-31 - 2021-01-13 | 711341 - 7720084 | 1 |
Sector Notes
Noted Issue | Description |
Scattered light | In Sector 33, the Moon introduces a strong glint in Camera 1 at the end of orbit 73. |
Sector 34 Information
For full data release notes see: DRN50. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 115.3 | -33.78 | 163.19 |
Camera 1 | 125.08 | 1.02 | 256.09 |
Camera 2 | 119.02 | -22.24 | 254.95 |
Camera 3 | 110.4 | -45.18 | 70.06 |
Camera 4 | 90.0 | -66.56 | 52.82 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
75 | 2021-01-14 - 2021-01-26 | 720929 - 729684 | 1 |
76 | 2021-01-27 - 2021-02-08 | 730459 - 739159 | 1 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | Camera 1 and Camera 4 were both used for guiding in orbit 75 of Sector 34. Camera 4 alone was used for guiding in orbit 76. |
Sector 35 Information
For full data release notes see: DRN51. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 133.2 | -39.69 | 152.4 |
Camera 1 | 149.12 | -6.65 | 248.97 |
Camera 2 | 139.52 | -28.87 | 245.98 |
Camera 3 | 124.58 | -50.03 | 56.29 |
Camera 4 | 90.0 | -66.56 | 26.32 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
77 | 2021-02-09 - 2021-02-21 | 739821 - 748579 | 1 |
78 | 2021-02-23 - 2021-03-06 | 749609 - 757817 | 1 |
Sector Notes
Noted Issue | Description |
Instrument issues | The spacecraft passed through the shadow of the Earth at the end of orbit 77. During this time, the instrument was turned off and no data were collected for 6.26 hours between TJD 2266.1091 and 2266.3700. The thermal state of the spacecraft changed during this time, and trends in the raw photometry and target positions are apparent after data collection resumed. |
Spacecraft pointing |
Approximately 40 minutes after the start of orbit 78, the spacecraft dropped out of Fine Pointing mode. For the next 3.44 days—between TJD 2268.5758 and 2272.0133—the spacecraft was in Coarse Pointing mode: in this mode, the spacecraft attitude drifts by about 1.5 pixels on timescales of 1 hour. Data continued to be collected while in Coarse Pointing: these data are flagged and removed from the PDCSAP FLUX light curves and transiting planet search. The FFIs are also flagged for Coarse Pointing. See the DRN Section 4.1 for more information about this.
Camera 4 alone was used for guiding in orbit 77 of Sector 35. Camera 1 and Camera 4 were both used for guiding in orbit 78. |
Scattered light | In Sector 35, there is scattered light at the beginning of both orbits. For orbit 77, the scattered light briefly saturates Camera 1. |
Sector 36 Information
For full data release notes see: DRN52. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 150.95 | -47.75 | 143.73 |
Camera 1 | 172.19 | -16.27 | 245.52 |
Camera 2 | 159.89 | -37.69 | 239.83 |
Camera 3 | 137.97 | -56.8 | 43.41 |
Camera 4 | 90.0 | -66.56 | 0.5 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
79 | 2021-03-07 - 2021-03-19 | 758479 - 767087 | 1 |
80 | 2021-03-20 - 2021-04-01 | 767759 - 776544 | 1 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | Camera 4 alone was used for guiding in orbits 79 and 80 of Sector 36. |
Scattered light | In Sector 36, there is scattered light at the beginning of both orbits. |
Sector 37 Information
For full data release notes see:DRN54. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 170.25 | -57.37 | 138.17 |
Camera 1 | 196.22 | -26.44 | 246.32 |
Camera 2 | 182.16 | -47.75 | 237.67 |
Camera 3 | 151.0 | -65.14 | 31.21 |
Camera 4 | 90.0 | -66.56 | 334.7 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
81 | 2021-04-02 - 2021-04-14 | 777441 - 785934 | 1 |
82 | 2021-04-15 - 2021-04-28 | 786793 - 795689 | 1 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | Both Cameras 1 and 4 were used for guiding in orbits 81 and 82 of Sector 37. |
Scattered light | In Sector 37, there is scattered light at the beginning of both orbits. |
Sector 38 Information
For full data release notes see: DRN55. For a list of TIC IDs with noted issues, see this list.
Update: The TESS Input Catalog was updated to v8.2. This new TIC identifies some newly discovered ARTIFACT and DUPLICATE sources that were not flagged in v8.0/8.1. For a description of these anomalies please read Section 1.1 of the DRN in addition to supplemental material.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 195.72 | -67.83 | 139.35 |
Camera 1 | 223.78 | -35.52 | 252.42 |
Camera 2 | 210.45 | -57.81 | 242.52 |
Camera 3 | 164.45 | -74.88 | 19.59 |
Camera 4 | 90.0 | -66.56 | 308.17 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
83 | 2021-04-29 - 2021-05-11 | 796604 - 805592 | 1 |
84 | 2021-05-12 - 2021-05-26 | 806284 - 815829 | 1 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | Camera 4 alone was used for guiding in orbit 83 of Sector 38. Both Cameras 1 and 4 were used for guiding in orbit 84. |
Scattered light | In Sector 38, there is scattered light for most of both orbits. |
Sector 39 Information
For full data release notes see: DRN56. For a list of TIC IDs with noted issues, see this list.
Update: The TESS Input Catalog was updated to v8.2. This new TIC identifies some newly discovered ARTIFACT and DUPLICATE sources that were not flagged in v8.0/8.1. For a description of these anomalies please read Section 1.1 of the DRN in addition to supplemental material.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 242.2 | -76.4 | 161.6 |
Camera 1 | 256.42 | -40.93 | 264.36 |
Camera 2 | 251.04 | -64.73 | 259.98 |
Camera 3 | 182.47 | -85.64 | 12.32 |
Camera 4 | 90.01 | -66.56 | 280.76 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
85 | 2021-05-27 - 2021-06-09 | 816704 - 826129 | 1 |
86 | 2021-06-10 - 2021-06-24 | 826849 - 836829 | 1 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | Cameras 1 and 4 were used for guiding in orbits 85 and 86 of Sector 39. |
Scattered light | In Sector 39, there is scattered light for most of both orbits. |
Sector 40 Information
For full data release notes see: DRN57. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 273.08 | 61.74 | 14.15 |
Camera 1 | 282.3 | 26.28 | 97.42 |
Camera 2 | 277.61 | 50.01 | 100.38 |
Camera 3 | 262.98 | 73.14 | 293.53 |
Camera 4 | 143.44 | 79.24 | 51.66 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
87 | 2021-06-25 - 2021-07-08 | 837499 - 847399 | 1 |
88 | 2021-07-09 - 2021-07-23 | 848066 - 857807 | 1 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | Both Cameras 1 and 4 were used for guiding in orbits 87 and 88 of Sector 40. |
Scattered light | In Sector 40, there is scattered light present for most of both orbits. |
Sector 41 Information
For full data release notes see: DRN59. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 277.62 | 62.76 | 37.22 |
Camera 1 | 301.95 | 30.34 | 108.71 |
Camera 2 | 289.56 | 52.55 | 117.09 |
Camera 3 | 254.91 | 70.99 | 328.21 |
Camera 4 | 180.26 | 68.99 | 39.45 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
89 | 2021-07-24 - 2021-08-06 | 858621 - 867704 | 1 |
90 | 2021-08-07 - 2021-08-20 | 868506 - 877769 | 1 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | Sector 41 consists of observations of the northern ecliptic hemisphere. For northern pointings, scattered light from the Earth and Moon is a more persistent issue for Camera 1 and Camera 2 than for southern pointings. For this reason, the spacecraft pointing was set at +85 degrees in ecliptic latitude, so that Camera 2 and Camera 3 straddle the ecliptic pole. Both Cameras 1 and 4 were used for guiding in orbits 89 and 90 of Sector 41. |
Scattered light | In Sector 41, there is scattered light present for most of both orbits. |
Sector 42 Information
For full data release notes see: DRN60. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 13.01 | 6.33 | 292.8 |
Camera 1 | 339.85 | -7.88 | 22.34 |
Camera 2 | 1.96 | 1.59 | 23.57 |
Camera 3 | 24.27 | 10.84 | 201.11 |
Camera 4 | 47.84 | 18.4 | 195.07 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
91 | 2021-08-21 - 2021-09-02 | 878566 - 887652 | 1 |
92 | 2021-09-03 - 2021-09-15 | 888321 - 896907 | 1 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | Sector 42 consists of observations of the ecliptic plane. For ecliptic pointings, the antisolar point is set towards the edge of Camera 1 (nearest Camera 2), and Cameras 2, 3, and 4 are aligned parallel to the ecliptic plane in the westward direction. Camera 4 alone was used for guiding in orbits 91 and 92 of Sector 42. |
Scattered light | In Orbit 91, the Moon crosses the fields of view of all cameras (one at a time), and the Earth crosses the fields of view of Cameras 1 and 2. The Moon and the Earth saturate CCD detectors during these times. Outside of these times, strong scattered light signals are also present for most of Orbit 91 and the second half of Orbit 92. |
Jupiter | Jupiter was near opposition during Sector 42, and landed in the field-of-view of Camera 1 for ∼7 days at the beginning of observations. Jupiter appears as a very bright object at the bottom of Camera 1, CCD 4, output channel A. It does not affect contrending for any targets on this CCD, although the smear correction for its associated columns is unreliable and targets close to Jupiter may have unreliable photometry for the first 7 days of observations. |
Sector 43 Information
For full data release notes see:DRN62. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 49.53 | 18.97 | 284.96 |
Camera 1 | 14.64 | 6.87 | 23.04 |
Camera 2 | 37.49 | 15.5 | 18.54 |
Camera 3 | 62.01 | 21.64 | 190.61 |
Camera 4 | 87.95 | 23.99 | 180.4 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
93 | 2021-09-16- 2021-09-28 | 897629 - 906244 | 1 |
94 | 2021-09-29 - 2021-10-11 | 906999 - 915432 | 1 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | Sector 43 consists of observations of the ecliptic plane. For ecliptic pointings, the antisolar point is set towards the edge of Camera 1 (nearest Camera 2), and Cameras 2, 3, and 4 are aligned parallel to the ecliptic plane in the westward direction. Camera 4 alone was used for guiding in orbits 93 and 94 of Sector 43. Outside of these times, strong scattered light signals are present when the Moon or Earth are near the camera fields of view. |
Scattered light | In Orbit 93, the Moon crosses the fields of view of all cameras (one at a time). The Moon saturates CCD detectors during these times. Outside of these times, strong scattered light signals are present when the Moon or Earth are near the camera fields of view. |
Anomalous effects | On Camera 3, CCD 1, ouput Channel D (columns greater than 1580), a small change to the start of frame ringing (cf. TESS Instrument Handbook, Section 6.8.2) was observed at row numbers ≲750. The change starts at TJD=2475.22927 in orbit 93, and is restricted to orbit 93. The amplitude is very small, only 0.27 electrons per second, and is usually corrected at the flux time series level during background subtraction for individual targets. However, the effect is not removed by the calibration model and is visible in raw/calibrated pixels in this region of the detector. See the DRN for more information. |
Sector 44 Information
For full data release notes see: DRN64. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 89.61 | 24.13 | 270.16 |
Camera 1 | 51.11 | 19.23 | 14.87 |
Camera 2 | 76.5 | 23.54 | 5.47 |
Camera 3 | 102.72 | 23.61 | 174.83 |
Camera 4 | 128.16 | 19.41 | 165.36 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
95 | 2021-10-12 - 2021-10-24 | 916364 - 924674 | 1 |
96 | 2021-10-25 - 2021-11-05 | 925734 - 933829 | 1 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | Sector 44 consists of observations of the ecliptic plane. For ecliptic pointings, the antisolar point is set towards the edge of Camera 1 (nearest Camera 2), and Cameras 2, 3, and 4 are aligned parallel to the ecliptic plane in the westward direction. Camera 1 alone was used for guiding in orbits 95 and 96 of Sector 44. |
Scattered light | At the end of orbit 95, the Moon crosses through Camera 1 and saturates the CCD detectors. At the start of orbit 96, the Moon is in Camera 3 and moves through Camera 4. Outside of these times, strong scattered light signals are present when the Moon or Earth are near the camera fields of view. |
Sector 45 Information
For full data release notes see: DRN65. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 130.3 | 19.02 | 255.09 |
Camera 1 | 91.85 | 23.99 | 359.67 |
Camera 2 | 117.81 | 21.67 | 349.45 |
Camera 3 | 142.33 | 15.56 | 161.5 |
Camera 4 | 165.2 | 6.93 | 156.97 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
97 | 2021-11-07 - 2021-11-19 | 934594 - 943577 | 1 |
98 | 2021-11-20 - 2021-12-02 | 944411- 952682 | 1 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | Sector 45 consists of observations of the ecliptic plane, with the camera array aligned along the ecliptic and Camera 1 the westernmost of the four. At the beginning of Sector 45, the center of Camera 1 was ∼ 50 degrees from the antisolar point; at the end of the sector, the distance was ∼ 23 degrees. Camera 1 alone was used for guiding in orbits 97 and 98 of Sector 45. |
Scattered light | At the start of orbit 97, the Earth crosses through Cameras 2, 3, and 4 and saturates the CCD detectors. At the start of orbit 98, the Earth is in Camera 4, while the Moon is in Camera 1 and moves through Camera 2. Outside of these times, strong scattered light signals are present when the Moon or Earth are near the camera fields of view. |
Sector 46 Information
Happy 100 orbit anniversary!
For full data release notes see: DRN66. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 157.7 | 10.09 | 248.41 |
Camera 1 | 121.93 | 20.78 | 348.27 |
Camera 2 | 146.19 | 14.28 | 340.85 |
Camera 3 | 168.9 | 5.51 | 156.88 |
Camera 4 | 190.92 | -4.08 | 156.6 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
99 | 2021-12-03 - 2021-12-16 | 953356 - 962757 | 1 |
100 | 2021-12-17 - 2021-12-30 | 963761 - 972897 | 1 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | Sector 46 consists of observations of the ecliptic plane, with the camera array aligned along the ecliptic and Camera 1 the westernmost of the four. Within the first 13 hours of orbit 99, Camera 4 alone was used for guiding. However, the Earth passed close enough to Camera 4 after this time that guiding was switched to Camera 1. The change in guiding was done in two steps. First, Camera 1 was enabled for guiding (concurrently with Camera 4) at TJD= 2552.088254 days. Then, Camera 4 was disabled for guiding 30 minutes later, at TJD= 2552.109087 days. At these two epochs, the spacecraft pointing shifted by a small amount, less than 1". The cadences for each data mode at these epochs are marked with an Attitude Tweak anomaly flag. In some cases, especially for saturated stars, the SAP FLUX light curves exhibit a step function at these times. Camera 1 alone was used for guiding in all of orbit 100. |
Scattered light | At the start of orbit 99, the Earth crosses through Cameras 1, 2, and 3, saturating the CCD detectors and/or causing strong glints. At the start of orbit 100, the Earth is in Camera 3 and saturates the detectors before moving close to the edge of Camera 4, while the Moon passes close to Camera 1. When the Earth or Moon are close to the camera fields of view, they cause strong glints and scattered light signals. |
Sector 47 Information
For full data release notes see: DRN67. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 143.38 | 73.11 | 327.1 |
Camera 1 | 119.09 | 39.11 | 78.27 |
Camera 2 | 129.33 | 62.28 | 70.17 |
Camera 3 | 187.34 | 80.64 | 194.1 |
Camera 4 | 270.0 | 66.56 | 113.37 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
101 | 2021-12-31 - 2022-01-13 | 973686 - 983162 | 1 |
102 | 2022-01-14 - 2022-01-27 | 983821 - 993229 | 1 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | Sector 47 consists of observations of the northern ecliptic hemisphere, with Camera 4 pointed near the north ecliptic pole. Camera 1 and Camera 4 were both used for guiding in orbit 101. Camera 4 alone was used for guiding in orbit 102. |
Scattered light | At the start of orbit 102, the Moon crosses through Camera 1, saturating the CCD detectors and causing strong glints in Camera 1 and 2. |
Sector 48 Information
For full data release notes see: DRN70. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 179.43 | 62.1 | 317.42 |
Camera 1 | 151.83 | 30.83 | 68.36 |
Camera 2 | 166.08 | 52.45 | 58.7 |
Camera 3 | 203.0 | 69.41 | 205.82 |
Camera 4 | 270.0 | 66.56 | 142.75 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
103 | 2022-01-28 - 2022-02-11 | 993941 - 1003804 | 1 |
104 | 2022-02-12 - 2022-02-25 | 1004821 - 1014142 | 1 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | Sector 48 consists of observations of the northern ecliptic hemisphere, with Camera 4 pointed near the north ecliptic pole. Camera 4 alone was used for guiding in both orbits. |
Scattered light | At the start of orbit 103, the Earth crosses through Cameras 1, saturating the CCD detectors and/or causing strong glints. At the start of orbit 104, the Earth and then the Moon moves through Camera 1, saturating the detectors and causing strong glints and scattered light signals in Cameras 1 and 2. |
Sector 49 Information
For full data release notes see: DRN71. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 202.64 | 50.95 | 321.35 |
Camera 1 | 179.67 | 19.82 | 65.28 |
Camera 2 | 192.72 | 41.1 | 58.53 |
Camera 3 | 217.48 | 59.54 | 219.1 |
Camera 4 | 270.0 | 66.56 | 171.55 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
105 | 2022-02-26 - 2022-03-11 | 1015209 - 1024552 | 1 |
106 | 2022-03-12 - 2022-03-25 | 1025249 - 1034539 | 1 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | Sector 49 consists of observations of the northern ecliptic hemisphere, with Camera 4 pointed near the north ecliptic pole. Camera 4 alone was used for guiding in both orbits. |
Scattered light | At the start of orbit 105, the Earth crosses through Camera 1, saturating the CCD detectors and/or causing strong glints. At the start of orbit 106, the Earth and then the Moon moves through Camera 1, saturating the detectors and causing strong glints and scattered light signals in Cameras 1 and 2. |
Sector 50 Information
For full data release notes see: DRN72. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 221.86 | 41.76 | 329.73 |
Camera 1 | 204.39 | 9.21 | 67.61 |
Camera 2 | 214.82 | 31.16 | 63.94 |
Camera 3 | 231.6 | 51.76 | 232.6 |
Camera 4 | 270.0 | 66.56 | 199.04 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
107 | 2022-03-26 - 2022-04-08 | 1035224 - 1044682 | 1 |
108 | 2022-04-09 - 2022-04-22 | 1045331 - 1054119 | 1 |
Sector Notes
Noted Issue | Description |
Data collection | Data collection was paused for four hours in orbit 107 (between TJD 2672.2512 and 2672.4206) to test data downlink near spacecraft apogee, in preparation for operation changes scheduled for 2022 September. |
Spacecraft pointing | Sector 50 consists of observations of the northern ecliptic hemisphere, with Camera 4 pointed near the north ecliptic pole. Camera 4 alone was used for guiding in the first half of orbit 107. After the data downlink at apogee, guiding with both Cameras 1 and 4 was enabled. This introduced a small shift in the spacecraft attitude in the second half of orbit 107. Some SAP FLUX light curves may show discontinuities before and after the data gap at these times. However, cotrending with PDC removes this offset in most cases. Camera 4 alone was used for guiding in all of orbit 108. |
Scattered light | At the start of orbit 107, the Earth crosses through Cameras 1 and 2, saturating the CCD detectors and/or causing strong glints. At the start of orbit 108, the Earth and then the Moon moves through Camera 1, saturating the detectors and causing strong glints and scattered light signals in both Cameras 1 and 2. |
Sector 51 Information
For full data release notes see: DRN74. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 239.43 | 35.23 | 339.87 |
Camera 1 | 227.75 | 0.91 | 73.67 |
Camera 2 | 234.94 | 23.88 | 72.09 |
Camera 3 | 245.38 | 46.36 | 245.95 |
Camera 4 | 270.0 | 66.56 | 225.02 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
109 | 2022-04-23 - 2022-05-05 | 1055151 - 1063612 | 1 |
110 | 2022-05-06 - 2022-05-18 | 1064321 - 1072857 | 1 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | Sector 51 consists of observations of the northern ecliptic hemisphere, with Camera 4 pointed near the north ecliptic pole. Camera 4 alone was used for guiding in both orbit 109 and orbit 110. |
Scattered light | The Earth is above the sunshade for extended periods of time in Sector 51, which results in high background levels and large gaps in the light curves. At the start of orbit 109 and orbit 110, the Earth crosses through Cameras 1 and 2, saturating the CCD detectors and/or causing strong glints. Throughout orbit 110, the Moon moves through Camera 1, saturating the detectors and causing strong glints and scattered light signals in both Cameras 1 and 2. |
Sector 52 Information
For full data release notes see: DNR76. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 266.36 | 61.82 | 343.14 |
Camera 1 | 255.37 | 26.58 | 81.19 |
Camera 2 | 260.96 | 50.2 | 77.65 |
Camera 3 | 278.24 | 72.97 | 242.12 |
Camera 4 | 30.09 | 78.17 | 131.93 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
111 | 2022-05-19 - 2022-05-30 | 1073646 - 1082049 | 1 |
112 | 2022-05-31 - 2022-06-12 | 1082871 - 1091247 | 1 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | Sector 52 consists of observations of the northern ecliptic hemisphere. The pointing was set at +85 degrees in ecliptic latitude so that Camera 2 and Camera 3 straddle the ecliptic pole. Camera 4 alone was used for guiding in both orbit 111 and 112. |
Scattered light | The Earth comes very close to the corner of the FOV of Camera 1 in the early part of both orbit 111 and orbit 112: the resulting scattered light saturates the CCD detectors in Camera 1. |
Sector 53 Information
For full data release notes see: DRN77. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 270.81 | 61.58 | 3.68 |
Camera 1 | 273.21 | 25.61 | 91.94 |
Camera 2 | 271.99 | 49.59 | 92.7 |
Camera 3 | 268.11 | 73.53 | 276.19 |
Camera 4 | 106.92 | 82.18 | 77.02 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
113 | 2022-06-13 - 2022-06-25 | 1091906 - 1100549 | 1 |
114 | 2022-06-26 - 2022-07-08 | 1101206 - 1109897 | 1 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | Sector 53 consists of observations of the northern ecliptic hemisphere. The pointing was set at +85 degrees in ecliptic latitude so that Camera 2 and Camera 3 straddle the ecliptic pole. Camera 4 alone was used for guiding in both orbit 113 and 114. |
Scattered light | In Sector 53, the Earth and Moon introduce scattered light signals throughout both orbits, with a strong scattered light signature in Camera 1 at the midpoint of both orbits. |
Sector 53 Information
For full data release notes see: DRN77. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 270.81 | 61.58 | 3.68 |
Camera 1 | 273.21 | 25.61 | 91.94 |
Camera 2 | 271.99 | 49.59 | 92.7 |
Camera 3 | 268.11 | 73.53 | 276.19 |
Camera 4 | 106.92 | 82.18 | 77.02 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
113 | 2022-06-13 - 2022-06-25 | 1091906 - 1100549 | 1 |
114 | 2022-06-26 - 2022-07-08 | 1101206 - 1109897 | 1 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | Sector 53 consists of observations of the northern ecliptic hemisphere. The pointing was set at +85 degrees in ecliptic latitude so that Camera 2 and Camera 3 straddle the ecliptic pole. Camera 4 alone was used for guiding in both orbit 113 and 114. |
Scattered light | In Sector 53, the Earth and Moon introduce scattered light signals throughout both orbits, with a strong scattered light signature in Camera 1 at the midpoint of both orbits. |
Sector 54 Information
For full data release notes see: DRN78. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 290.12 | 32.61 | 13.46 |
Camera 1 | 297.99 | -2.61 | 101.32 |
Camera 2 | 293.09 | 20.9 | 102.11 |
Camera 3 | 286.25 | 44.22 | 285.87 |
Camera 4 | 270.01 | 66.56 | 299.53 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
115 | 2022-07-09 - 2022-07-21 | 1110556 - 1119515 | 1 |
116 | 2022-07-23 - 2022-08-04 | 1120371 - 1129445 | 1 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | The pointing in Sector 54 was set at +54 degrees in ecliptic latitude, so that Camera 4 was pointed at the North Ecliptic Pole. Camera 4 alone was used for guiding in both orbit 115 and 116. |
Scattered light | In Sector 54, the Earth and Moon introduce scattered light signals throughout both orbits, and saturate the detectors as they cross through Camera 1 in the second half of each orbit. |
Sector 55 Information
For full data release notes see: DRN79. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 307.87 | 37.65 | 24.54 |
Camera 1 | 322.03 | 4.06 | 109.25 |
Camera 2 | 313.41 | 26.6 | 111.58 |
Camera 3 | 300.4 | 48.35 | 299.65 |
Camera 4 | 270.0 | 66.57 | 325.77 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
117 | 2022-08-05 - 2022-08-18 | 1130141 - 1139402 | 1 |
118 | 2022-08-19 - 2022-09-01 | 1140056 - 1149702 | 1 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | The pointing in Sector 55 was set at +54 degrees in ecliptic latitude so that Camera 4 was pointed at the North Ecliptic Pole. Camera 4 alone was used for guiding in both orbit 117 and 118. |
Scattered light | In Sector 55, the Earth and Moon introduce scattered light signals throughout the observations, with the strongest signals in the second half of both orbits. The Moon crosses through Camera 1 in the first orbit. |
Sector 56 Information
For full data release notes see: DRN80. For a list of TIC IDs with noted issues, see this list.
Update: DR80 is the first data release of the second TESS extended mission, in which the FFI data collection interval has been reduced to 200 seconds. As in the primary mission and first extended mission, select pixel stamps were collected at 2-minute cadence and 20-second cadence. The number of targets in each data mode were adjusted: 13,000 targets were selected for 2-minute cadence observations, while all observable 20-second cadence targets were selected.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 324.28 | 46.34 | 36.25 |
Camera 1 | 345.36 | 14.96 | 114.99 |
Camera 2 | 333.05 | 36.3 | 120.43 |
Camera 3 | 311.76 | 55.43 | 316.01 |
Camera 4 | 266.08 | 65.86 | 356.48 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
119a | 2022-09-02 - 2022-09-09 | 1150414 - 1155075 | 1 |
119b | 2022-09-09 - 2022-09-16 | 1155226 - 1159962 | |
120a | 2022-09-16 - 2022-09-23 | 1160114 - 1165265 | 1 |
120b | 2022-09-23 - 2022-09-30 | 1165414 - 1170492 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | The pointing in Sector 56 was set at +55.5◦ in ecliptic latitude. As a result, Camera 4 was pointed near, but not exactly at the North Ecliptic Pole. The slight offset in target declination was introduced in the second Extended Mission to allow observations of the North Ecliptic Pole itself, which has fallen in the gaps between CCDs in the Prime Mission and first Extended Mission. Camera 1 and Camera 4 were used for guiding in both orbit 119 and 120, except for the second half of orbit 119 in which Camera 4 alone was used for guiding. |
Scattered light | In Sector 56, the Moon introduces scattered light signals towards the second half of orbit 1. |
Cosmic rays | Cosmic rays were mitigated in the 2-minute cadence data and 200-second FFIs by analgorithm running on the instrument firmware, in the same way as in the primary mission and first extended mission. For the 20-second cadence data, cosmic rays were identified and corrected in SPOC data processing, in the same way as the first extended mission. See DRN38 for details. |
Sector 57 Information
For full data release notes see: DRN82. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 344.23 | 56.41 | 44.01 |
Camera 1 | 11.28 | 26.11 | 115.34 |
Camera 2 | 356.47 | 47.06 | 124.35 |
Camera 3 | 325.1 | 63.84 | 330.67 |
Camera 4 | 267.38 | 65.2 | 23.58 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
121a | 2022-09-30 - 2022-10-08 | 1170644 - 1175847 | 1 |
121b | 2022-10-08 - 2022-10-14 | 1175999 - 1180650 | |
122a | 2022-10-14 - 2022-10-22 | 1180801 - 1185950 | 1 |
122b | 2022-10-22 - 2022-10-29 | 1186101 - 1191355 |
Sector Notes
Noted Issue | Description |
Safe mode | At TJD 2863.28, the spacecraft entered into safe mode, resulting in instrument turn-off until TJD 2866.41. There are no FFIs, target pixel file data, or light curve data during this time. During these times (as well as when the spacecraft is transmitting data to ground systems) the data and timestamps in target-pixel files and light curve files are set to NULL. |
Spacecraft pointing | The pointing in Sector 57 was set at +54 degrees in ecliptic latitude so, so that Camera 4 was pointed at the North Ecliptic Pole. Camera 1 and Camera 4 alone were used for guiding in both orbit 121 and 122, except for the second half of orbit 121 in which Camera 4 alone was used for guiding. |
Scattered light | In Sector 57, the Moon introduces scattered light signals towards the second half of orbit 1. |
Sector 58 Information
For full data release notes see: DRN83. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 9.31 | 67.65 | 45.36 |
Camera 1 | 40.55 | 36.24 | 109.6 |
Camera 2 | 25.58 | 58.12 | 120.81 |
Camera 3 | 337.32 | 73.79 | 345.69 |
Camera 4 | 269.23 | 64.86 | 50.44 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
123a | 2022-10-29 - 2022-11-05 | 1191506 - 1196617 | 1 |
123b | 2022-11-06 - 2022-11-12 | 1196769 - 1201392 | |
124a | 2022-11-12 - 2022-11-19 | 1201544 - 1206670 | 1 |
124b | 2022-11-20 - 2022-11-26 | 1206821 - 1211467 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | The pointing in Sector 58 was set at +55.5 degrees in ecliptic latitude. Camera 1 and Camera 4 alone were used for guiding in both orbit 123 and 124. |
Scattered light | In Sector 58, the Moon introduces scattered light signals towards the second half of orbit 1. |
Sector 59 Information
For full data release notes see: DRN84. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 52.98 | 77.17 | 26.51 |
Camera 1 | 73.73 | 42.23 | 97.69 |
Camera 2 | 66.08 | 65.85 | 104.01 |
Camera 3 | 344.03 | 84.29 | 4.86 |
Camera 4 | 271.19 | 64.9 | 76.49 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
125a | 2022-11-26 - 2022-12-03 | 1211619 - 1216287 | 1 |
125b | 2022-12-03 - 2022-12-09 | 1216439 - 1221042 | |
126a | 2022-12-10 - 2022-12-16 | 1221194 - 1226032 | 1 |
126b | 2022-12-16 - 2022-12-23 | 1226184 - 1230647 |
Sector Notes
Noted Issue | Description |
Processing issue | Sector 59 data were briefly made available on 2023 January 18–19 before an issue was identified that required reprocessing. Data have since been reprocessed. The reprocessing has a minimal impact on the final light curves, but resulted in a different set of TCEs than initially released. Users should re-download the data if retrieved before January 19th, 2023. |
Spacecraft pointing | The pointing in Sector 59 was set at +55.5 degrees in ecliptic latitude. Camera 1 and Camera 4 alone were used for guiding in both orbit 125 and 126. |
Scattered light | In Sector 59, the Earth introduces scattered light signals at the very start of each orbit. |
Sector 60 Information
For full data release notes see: DRN85. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 125.67 | 77.31 | 337.32 |
Camera 1 | 107.9 | 42.08 | 83.45 |
Camera 2 | 114.4 | 65.8 | 78.08 |
Camera 3 | 196.61 | 85.14 | 176.9 |
Camera 4 | 272.86 | 65.28 | 101.68 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
127a | 2022-12-23 - 2022-12-30 | 1230799 - 1235700 | 1 |
127b | 2022-12-30 - 2023-01-05 | 1235851 - 1240065 | |
128a | 2023-01-05 - 2023-01-11 | 1240216 - 1244727 | 1 |
128b | 2023-01-11 - 2023-01-18 | 1244879 - 1249292 |
Sector Notes
Noted Issue | Description |
Safe mode | At TJD 2949.99, the spacecraft entered into safe mode, resulting in instrument turn-off until TJD 2955.04. There are no FFIs, target pixel file data, or light curve data during this time. During these times (as well as when the spacecraft is transmitting data to ground systems) the data and timestamps in target-pixel files and light curve files are set to NULL. One FFI from Camera 1 in orbit 127 was corrupted prior to downlink from the spacecraft and could not be recovered. The FFIINDEX number is 00738895 (timestamp 2022358084201), and no FFI file for Camera 1 was produced for this cadence. |
Spacecraft pointing | The pointing in Sector 60 was set at +55.5 degrees in ecliptic latitude. Camera 4 alone was used for guiding in the first half of orbit 127. Camera 1 and Camera 4 were both used for guiding at all other times. |
Scattered light | In Sector 60, the Earth introduces scattered light signals at the very start of each orbit. |
Sector 61 Information
For full data release notes see: DRN86. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 118.04 | -36.09 | 162.22 |
Camera 1 | 128.39 | -1.39 | 255.71 |
Camera 2 | 122.05 | -24.59 | 254.25 |
Camera 3 | 112.66 | -47.41 | 68.62 |
Camera 4 | 89.06 | -68.26 | 48.23 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
129a | 2023-01-18 - 2023-01-24 | 1249444 - 1254152 | 1 |
129b | 2023-01-25 - 2023-01-30 | 1254304 - 1258375 | |
130a | 2023-01-30 - 2023-02-06 | 1258526 - 1263410 | 1 |
130b | 2023-02-06 - 2023-02-12 | 1263561 - 1267755 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | The pointing in Sector 61 was set at −55.5 degrees in ecliptic latitude. Camera 4 alone was used for guiding in the first half of orbit 129 and orbit 130. Camera 1 and Camera 4 were both used for guiding in the second half of each orbit. |
Scattered light | In Sector 61, the Earth introduces scattered light signals at the start and end of each orbit. |
Sector 62 Information
For full data release notes see: DRN88. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 135.24 | -42.24 | 151.59 |
Camera 1 | 151.7 | -9.27 | 249.09 |
Camera 2 | 141.9 | -31.48 | 245.6 |
Camera 3 | 125.9 | -52.46 | 54.68 |
Camera 4 | 87.19 | -67.91 | 20.49 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
131a | 2023-02-12 - 2023-02-19 | 1267906 - 1272547 | 1 |
131b | 2023-02-19 - 2023-02-25 | 1272699 - 1276897 | |
132a | 2023-02-25 - 2023-03-04 | 1277049 - 1281657 | 1 |
132b | 2023-03-04 - 2023-03-10 | 1281809 - 1286422 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | The pointing in Sector 62 was set at −55.5 degrees in ecliptic latitude. Camera 1 and Camera 4 were both used for guiding in both orbits. |
Scattered light | In Sector 62, the Earth introduces scattered light signals at the start and end of each orbit. |
Sector 63 Information
For full data release notes see: DRN89. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 153.06 | -50.7 | 142.74 |
Camera 1 | 175.21 | -19.25 | 246.03 |
Camera 2 | 162.62 | -40.7 | 239.61 |
Camera 3 | 138.7 | -59.51 | 40.9 |
Camera 4 | 85.97 | -67.27 | 353.01 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
133a | 2023-03-10 - 2023-03-17 | 1286574 - 1291487 | 1 |
133b | 2023-03-17 - 2023-03-23 | 1291639 - 1295955 | |
134a | 2023-03-24 - 2023-03-30 | 1296106 - 1300777 | 1 |
134b | 2023-03-30 - 2023-04-06 | 1300929 - 1305680 |
Sector Notes
Noted Issue | Description |
Configuration error | Due to a configuration error, in Sector 63 the Earth Point flags (data quality bit 4) were not set during the download periods from Orbit 133a to 133b and Orbit 134a to 134b. However, there is no data during this time and values in the target pixel files and light curves are set to NULL. |
Spacecraft pointing | The pointing in Sector 63 was set at −55.5 degrees in ecliptic latitude. Camera 1 and Camera 4 were both used for guiding in Orbit 133a, 133b, and 134a, while Camera 4 alone was used for guiding in Orbit 134b. |
Scattered light | In Sector 63, the Moon introduces strong scattered light signals in Camera 1 at the start of Orbit 133 and end of Orbit 134. |
Sector 64 Information
For full data release notes see: DRN90. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 173.27 | -60.86 | 137.28 |
Camera 1 | 200.61 | -29.76 | 247.64 |
Camera 2 | 186.29 | -51.26 | 238.14 |
Camera 3 | 150.9 | -68.24 | 27.0 |
Camera 4 | 85.66 | -66.48 | 325.85 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
135a | 2023-04-06 - 2023-04-13 | 1305831 - 1310876 | 1 |
135b | 2023-04-13 - 2023-04-20 | 1311026 - 1315890 | |
136a | 2023-04-20 - 2023-04-27 | 1316041 - 1321030 | 1 |
136b | 2023-04-27 - 2023-05-03 | 1321181 - 1325215 |
Sector Notes
Noted Issue | Description |
Configuration error | Due to a configuration error, in Sector 64 the Earth Point flags (data quality bit 4) were not set during the download periods from Orbit 135a to 135b and Orbit 136a to 136b. However, there is no data during this time and values in the target pixel files and light curves are set to NULL. A configuration change on the spacecraft at UTC 2023-04-20-06:05:04 required the instrument to pass over one FFI, one 2-minute cadence, and one 20-second. There is no data at this time—the missing cadence numbers are 789392 (FFI), 1315656 (2-minute), and 7893937 (20-second). The spacecraft dropped into coarse pointing during this configuration change, and settles into fine pointing over the next 40 seconds. |
Spacecraft pointing | The pointing in Sector 64 was set at −55.5 degrees in ecliptic latitude. Camera 1 and Camera 4 were both used for guiding in Orbit 135a, 135b, and 136a, while Camera 4 alone was used for guiding in Orbit 136b. |
Sector 65 Information
For full data release notes see: DRN91. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 201.62 | -71.57 | 140.74 |
Camera 1 | 230.04 | -38.58 | 255.17 |
Camera 2 | 217.52 | -61.29 | 245.39 |
Camera 3 | 161.56 | -78.2 | 11.91 |
Camera 4 | 86.29 | -65.7 | 299.08 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
137a | 2023-05-04 - 2023-05-11 | 1325721 - 1330930 | 1 |
137b | 2023-05-11 - 2023-05-18 | 1331081 - 1336335 | 1 |
138a | 2023-05-19 - 2023-05-25 | 1336486 - 1341215 | 1 |
138b | 2023-05-25 - 2023-06-01 | 1341366 - 1345805 | 1 |
Sector Notes
Noted Issue | Description |
Anomalous detector voltage change |
Beginning 2023-05-19 13:54 UTC (3084.1 TJD) and lasting 3.4 days, Camera 4, CCD 4 experienced an anomalous detector voltage change leading to a 70% gain and 0.5◦ temperature change. After a commanded instrument reset, data collection resumed at the nominal operating conditions with no lasting impact due to the anomaly. The anomaly did not affect spacecraft fine pointing. No other cameras or CCDs were affected. Camera 4, CCD 4 FFI data during this time is not available on the MAST archive. FFI data for all other Cameras and CCDs were not impacted by the anomaly and are available on the MAST archive. For 2-min and 20-sec data products (TPF & LC), the Bad Calibration Exclude data quality flag (bit 15) is set for targets on Camera 4, CCD 4 during the 3.4-day anomaly, and these cadences were not used for PDC CBVs or the planet search in TPS and DV. Non-NULL pixel data present in TPFs for Camera 4, CCD 4 during the 3.4-day anomaly should be regarded as not calibrated and not suitable for scientific analysis using standard techniques. |
Configuration error | Due to a configuration error, the Earth Point flags in Sector 65 were not set during the download periods from Orbit 137a to 137b and Orbit 138a to 138b. However, there is no data during this time and values in the target pixel files and light curves are set to NULL. Off-nominal data downlink contacts resulted in the instrument solid state recorder filling to capacity. In this case, old data is maintained and new data is not recorded. Overall, 17 hours of observations at the end Orbit 138 were not recorded. |
Spacecraft pointing | The pointing in Sector 65 was set at −55.5 degrees in ecliptic latitude. Camera 1 and Camera 4 were both used for guiding in Orbit 137a, 137b, and 138a, while Camera 4 alone was used for guiding in Orbit 138b. |
Sector 66 Information
For full data release notes see: DRN92. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 259.17 | -78.8 | 173.91 |
Camera 1 | 264.05 | -42.85 | 268.39 |
Camera 2 | 262.38 | -66.83 | 267.0 |
Camera 3 | 139.09 | -88.54 | 323.95 |
Camera 4 | 87.69 | -65.11 | 272.81 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
139a | 2023-06-02 - 2023-06-09 | 1346554 - 1351752 | 1 |
139b | 2023-06-09 - 2023-06-16 | 1351904 - 1356855 | 1 |
140a | 2023-06-16 - 2023-06-23 | 1357006 - 1361967 | 1 |
140b | 2023-06-23 - 2023-06-30 | 1362089 - 1367260 | 1 |
Sector Notes
Noted Issue | Description |
Engineering tests | Beginning 2023-06-28 17:44 UTC (3124.224 TJD) until the end of the sector (2.2 day duration), TESS performed engineering tests. Pointing performance was highly variable during the engineering tests. Data during the engineering test is available on MAST archive. The Manual Exclude data quality flag (bit 8) is set in the FFI, 2-min, and 20-sec data products during the engineering test. Data during the engineering test was excluded for analysis in PDC, TPS, and DV. |
Fine Pointing mode issue | At 2023-06-27 14:28 UTC (3123.105 TJD), for 1 minute, the spacecraft dropped out of Fine Pointing mode, and the spacecraft subsequently self-recovered back into Fine Pointing mode. Data continued to be collected while in Coarse Pointing: these data are flagged and removed from the PDCSAP FLUX light curves and transiting planet search. The FFIs are also flagged for Coarse Pointing. |
Spacecraft pointing | The pointing in Sector 66 was set at −55.5 degrees in ecliptic latitude. Camera 1 and Camera 4 were both used for guiding in Orbit 139a and 140a, while Camera 4 alone was used for guiding in Orbit 139b and 140b. Pointing performance during the engineering testing (>3124.2 TJD) is highly variable, and the PDC, TPS, and DV modules ignored data beyond this timestamp; the manual exclude data quality flag (bit 8) also identifies data impacted by the engineering test. |
Scattered light | In Sector 66, the Earth introduces scattered light signals at the end of each orbit, and the Moon strongly impacts Camera 1 at the end of Orbit 140. |
Sector 67 Information
For full data release notes see: DRN94. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 326.77 | -74.28 | 217.47 |
Camera 1 | 298.62 | -40.72 | 282.56 |
Camera 2 | 310.15 | -63.75 | 291.88 |
Camera 3 | 16.76 | -80.49 | 176.45 |
Camera 4 | 89.51 | -64.84 | 247.19 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
141a | 2023-07-01 - 2023-07-07 | 1367411 - 1372075 | 1 |
141b | 2023-07-07 - 2023-07-14 | 1372226 - 1377212 | 1 |
142a | 2023-07-14 - 2023-07-22 | 1377364 - 1382580 | 1 |
142b | 2023-07-22 - 2023-07-28 | 1382731 - 1387397 | 1 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing | The pointing in Sector 67 was set at −55.5 degrees in ecliptic latitude. Camera 1 and Camera 4 were both used for guiding in Orbit 141a and 142a, while Camera 4 alone was used for guiding in Orbit 141b and 142b. |
Scattered light | In Sector 67, the Earth introduces scattered light signals at the end of each orbit, and the Moon strongly impacts Camera 1 at the end of Orbit 142. |
Sector 68 Information
For full data release notes see: DRN95. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 359.28 | -64.24 | 226.1 |
Camera 1 | 328.77 | -33.46 | 292.05 |
Camera 2 | 344.18 | -54.91 | 303.01 |
Camera 3 | 26.18 | -70.66 | 161.04 |
Camera 4 | 91.37 | -64.93 | 222.35 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
143a | 2023-07-29 - 2023-08-05 | 1387549 - 1392707 | 1 |
143b | 2023-08-05 - 2023-08-11 | 1392859 - 1397387 | 1 |
144a | 2023-08-11 - 2023-08-18 | 1397539 - 1402250 | 1 |
144b | 2023-08-18 - 2023-08-25 | 1402371 - 1407372 | 1 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing: | The pointing in Sector 68 was set at −55.5 degrees in ecliptic latitude. Camera 1 and Camera 4 were both used for guiding in Orbit 143a and 144a, while Camera 4 alone was used for guiding in Orbit 143b and 144b. |
Scattered light: | In Sector 68, the Earth introduces scattered light signals at the end of each orbit. |
Sector 69 Information
For full data release notes see: DRN96. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 20.04 | -54.23 | 222.77 |
Camera 1 | 354.17 | -23.84 | 295.72 |
Camera 2 | 8.57 | -44.78 | 304.0 |
Camera 3 | 37.54 | -61.99 | 147.69 |
Camera 4 | 92.95 | -65.32 | 198.11 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
145a | 2023-08-25 - 2023-08-31 | 1407524 - 1411725 | 1 |
Engineering mode | 2023-08-25 - 2023-08-27 | 1407524 - 1408949 | |
Observations resume | 2023-08-27 | 1408968 | |
145b | 2023-08-31 - 2023-09-07 | 1411876 - 1416627 | 1 |
146a | 2023-09-07 - 2023-09-14 | 1416779 - 1421322 | 1 |
146b | 2023-09-14 - 2023-09-20 | 1421474 - 1426092 | 1 |
Sector Notes
Noted Issue | Description |
Engineering tests: | At the beginning of the first orbit TESS performed engineering tests lasting ∼2 days. Five intervals during this time (lasting a total of ∼ 6.3 hr) where the spacecraft pointing was subject to impulses have the Manual Exclude (bit 8) data quality flag set in the 2-min and 20-sec data products. Data with Manual Exclude data quality flag are excluded for analysis in PDC, TPS, and DV. The FFI data products have the Manual Exclude data quality flag set during the entire duration of the 2 day engineering test because the FFIs were processed before the impact of the spacecraft pointing behavior was analyzed. Users can recover valid FFI data in the intervals given in Table 1 of DRN 96, which are consistent with the periods of good data in the 2-min and 20-sec data products. |
Data gap: | After the 2 day engineering test, data collection was paused for 36 min in order to reconfigure the spacecraft for normal operations. During the reconfiguration duration, no data quality flags are set; however, there are no data collected during this time. Values in the target pixel files and light curves are set to NULL during the reconfiguration. |
Corrupted data: | One FFI from Cameras 1 and 2 in orbit 145 was corrupted prior to downlink from the spacecraft and could not be recovered. The FFIINDEX number is 00849522, and no FFI file for Camera 1 and 2 was produced for this cadence. One FFI from Camera 1 in orbit 146 was corrupted prior to downlink from the spacecraft and could not be recovered. The FFIINDEX number is 00855522, and no FFI file for Camera 1 was produced for this cadence. |
Spacecraft pointing: | The pointing in Sector 69 was set at −55.5 degrees in ecliptic latitude. During the 2 day engineering test, all cameras were used for guiding. After observations resumed, Camera 1 and Camera 4 were both used for guiding in Orbit 145a and 146a, while Camera 4 alone was used for guiding in Orbit 145b and 146b. |
Scattered light: | In Sector 69 the Earth introduces scattered light signals at the end of each orbit. |
Sector 70 Information
For full data release notes see: DRN99. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 24.04 | 9.26 | 291.3 |
Camera 1 | 350.71 | -4.62 | 22.7 |
Camera 2 | 12.83 | 4.76 | 22.67 |
Camera 3 | 35.53 | 13.41 | 199.03 |
Camera 4 | 59.67 | 19.93 | 192.0 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
147a | 2023-09-20 - 2023-09-27 | 1426244 - 1430705 | 1 |
147b | 2023-09-27 - 2023-10-03 | 1430856 - 1435442 | 1 |
148a | 2023-10-03 - 2023-10-09 | 1435594 - 1439990 | 1 |
148b | 2023-10-10 - 2023-10-16 | 1440141 - 1444582 | 1 |
Sector Notes
Noted Issue | Description |
Saturated/Bleeding columns: | Jupiter is in the field of view of Camera 3 CCD 3 resulting in several saturated/bleeding columns (around 2018 column number) throughout the sector. |
Spacecraft pointing: | The pointing in Sector 70 was set at -0.7 degrees in ecliptic latitude with the cameras aligned parallel to the ecliptic plane. Camera 1 and then Camera 4 were individually used for guiding in Orbits 147a and 148a, respectively. Camera 1 was used for guiding in Orbit 147b and Cameras 1 and 4 in 148b. |
Scattered light: | In Sector 70, the Earth introduces scattered light signals at the end of each orbit, and the Moon strongly impacts all cameras at the end of Orbit 147. |
Sector 71 Information
For full data release notes see: DRN100 For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 77.34 | 22.22 | 275.0 |
Camera 1 | 40.03 | 14.98 | 17.32 |
Camera 2 | 64.55 | 20.68 | 9.69 |
Camera 3 | 90.32 | 22.75 | 180.02 |
Camera 4 | 116.1 | 20.69 | 170.34 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
149a | 2023-10-16 - 2023-10-22 | 1444734 - 1449387 | 1 |
149b | 2023-10-23 - 2023-10-29 | 1449539 - 1454077 | 1 |
150a | 2023-10-29 - 2023-11-04 | 1454229 - 1458660 | 1 |
150b | 2023-11-05 - 2023-11-11 | 1458811 - 1463410 | 1 |
Sector Notes
Noted Issue | Description |
Jupiter: | Jupiter enters the field of view of Camera 1 CCD 4 midway through orbit 149a (TJD ∼3237.82; Cadence Number 1447460). Jupiter’s appearance on the detector severely contaminates the trailing/leading black and smear calibration regions for the slice A readout columns (Columns 45 – 556), and the calibration of slice A is compromised for the entire sector. As a result of Jupiter’s light spilling into the calibration regions, the trailing/leading black levels fit along detector rows and the smear estimate fit along detector columns exhibit strong spatial gradients. Targets and FFI data on the Camera 1 CCD 4 slice A readout region are not correctly calibrated. The remaining readout slice B, C, D (columns 557 – 2092) regions for Camera 1 CCD 4 are not impacted by the calibration issues due to Jupiter. Data quality flags in the target and FFI data products for this region do not indicate when the calibration is compromised on slice A. Targets on this slice have unreliable photometry. |
Spacecraft pointing: | The pointing in Sector 71 was set at -0.7 degrees in ecliptic latitude with the cameras aligned parallel to the ecliptic plane. Camera 1 and then Camera 4 were individually used for guiding in Orbits 149a and 149b, respectively. Camera 1 was used for guiding in Orbit 150a and Cameras 1 and 4 in 150b. |
Scattered light: | In Sector 71, the Earth introduces scattered light signals at the beginning of each orbit, and the Moon strongly impacts all cameras at the end of Orbit 149 and beginning of Orbit 150. |
Sector 72 Information
For full data release notes see: DRN102. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 133.76 | 16.65 | 254.03 |
Camera 1 | 95.97 | 22.75 | 357.22 |
Camera 2 | 121.51 | 19.58 | 347.85 |
Camera 3 | 145.6 | 13.03 | 160.99 |
Camera 4 | 168.29 | 4.41 | 157.49 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
151a | 2023-11-11 - 2023-11-17 | 1463561 - 1468002 | 1 |
151b | 2023-11-18 - 2023-11-24 | 1468154 - 1472792 | 1 |
152a | 2023-11-24 - 2023-11-30 | 1472944 - 1477347 | 1 |
152b | 2023-12-01 - 2023-12-07 | 1477499 - 1481852 | 1 |
Sector Notes
Noted Issue | Description |
Corrupted data: | One FFI from Camera 2 in orbit 151 was corrupted prior to downlink from the spacecraft and could not be recovered. The FFIINDEX number is 878254, and no FFI file for Camera 2 was produced for this cadence. |
Spacecraft pointing: | The pointing in Sector 72 was set at -0.7 degrees in ecliptic latitude with the cameras aligned parallel to the ecliptic plane. Camera 1 was used for guiding in Orbit 151a and Cameras 1 and 4 were used in Orbit 151b. Camera 1 was used for guiding in Orbit 152a and Cameras 1 and 4 in 152b. |
Scattered light: | In Sector 72, the Earth introduces scattered light signals at the beginning of each orbit, and the Moon impacts Camera 4 at the end of Orbit 152. |
Sector 73 Information
For full data release notes see: DRN103. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 80.67 | 78.83 | 8.03 |
Camera 1 | 87.11 | 42.92 | 92.12 |
Camera 2 | 84.92 | 66.89 | 93.95 |
Camera 3 | 327.32 | 88.19 | 31.22 |
Camera 4 | 271.88 | 65.01 | 86.33 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
153a | 2023-12-07 - 2023-12-13 | 1482004 - 1486665 | 1 |
153b | 2023-12-13 - 2023-12-20 | 1486816 - 1491470 | 1 |
154a | 2023-12-20 - 2023-12-25 | 1491621 - 1494980 | 1 |
154b | 2023-12-27 - 2024-01-03 | 1496691 - 1501340 | 1 |
Sector Notes
Noted Issue | Description |
Data downlink: | Offnominal data downlink contacts resulted in the instrument solid state recorder (SSR) filling to capacity. Once the SSR reaches capacity, old data is maintained and new data is not recorded. Due to SSR fill, 2.16 days of observations at the end of 154a were not recorded. |
Spacecraft pointing: | The pointing in Sector 73 was set at +55.5 degrees in ecliptic latitude so that Camera 4 was pointed at the North Ecliptic Pole. Camera 4 was used for guiding in Orbit 153a and Cameras 1 and 4 were used in Orbit 153b. Camera 4 was used for guiding in Orbits 154a and b. |
Scattered light: | In Sector 73, the Earth introduces scattered light signals at the beginning of each orbit, and the Moon impacts Cameras 1 and 2 near the beginning of Orbit 154. |
Sector 74 Information
For full data release notes see: DRN105. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 261.22 | 72.3 | 213.92 |
Camera 1 | 137.52 | 66.78 | 64.51 |
Camera 2 | 220.12 | 79.83 | 343.99 |
Camera 3 | 275.32 | 61.57 | 110.87 |
Camera 4 | 286.0 | 38.5 | 102.52 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
155a | 2024-01-03 - 2024-01-09 | 1482004 - 1486665 | 1 |
155b | 2024-01-09 - 2024-01-16 | 1506249 - 1510842 | 1 |
156a | 2024-01-16 - 2024-01-23 | 1510994 - 1515955 | 1 |
156b | 2024-01-23 - 2024-01-30 | 1516076 - 1520722 | 1 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing: | The pointing in Sector 74 was set at +83.5 degrees in ecliptic latitude so that Camera 3 points near the North Ecliptic Pole. Camera 4 was used for guiding in Orbits 155a and 156a. Cameras 1 and 4 were used in Orbits 155b and 156b. |
Scattered light: | In Sector 74, the Earth introduces scattered light signals at the beginning of each orbit, and the Moon impacts Camera 1 near the beginning of Orbit 156. |
Sector 75 Information
For full data release notes see: DRN106. For a list of TIC IDs with noted issues, see this list.
Sector Summary
Spacecraft Pointing (deg)
RA | dec | roll | |
---|---|---|---|
Spacecraft | 254.93 | 69.94 | 247.49 |
Camera 1 | 171.87 | 56.84 | 54.6 |
Camera 2 | 218.55 | 71.1 | 11.91 |
Camera 3 | 280.01 | 63.06 | 134.38 |
Camera 4 | 302.93 | 43.06 | 115.7 |
Orbit Summary
Orbits | Dates (UTC) Start - End |
Cadence # Start - End |
Momentum dumps |
---|---|---|---|
157a | 2024-01-30 - 2024-02-05 | 1520874 - 1525480 | 1 |
157b | 2024-02-05 - 2024-02-13 | 1525631 - 1530792 | 1 |
158a | 2024-02-13 - 2024-02-19 | 1530944 - 1535520 | 1 |
158b | 2024-02-19 - 2024-02-26 | 1535671 - 1540820 | 1 |
Sector Notes
Noted Issue | Description |
Spacecraft pointing: | The pointing in Sector 75 was set at +83.5 degrees in ecliptic latitude so that Camera 3 points near the North Ecliptic Pole. Camera 4 was used for guiding in Orbits 157a and 158a. Cameras 1 and 4 were used in Orbits 157b and 158b. |
Scattered light: | In Sector 75, the Earth introduces scattered light signals after the beginning of each orbit, and the Moon impacts Camera 1 near the middle of Orbit 158. |