NASA  LDOPE
Error
Opening Date: 2024-04-10   Last update: 2024-04-16   Status: Note

The NOAA-20 satellite underwent a rephasing maneuver between March 20th, 2024 - April 4th, 2024, as part of an orbit rephasing to provide 180 degrees of separation between NOAA-20 and NOAA-21. The Satellite remained in Mission Pointing Mode during the drift period, which lasted for 16 days. The first propulsive burn maneuver successfully completed on March 20th, 2024, and lowered the NOAA-20's altitude to a lower orbit. The satellite drifted for 16 days, until positioned to 180 degrees from NOAA-21, after which another propulsive burn was performed successfully on April 4th, 2024, to raise the satellite back to its nominal orbit. The Land products were not made available, as all operational processing was suspended for the duration. The data production continued in a test archive set for review of data by VCST, Geolocation, and Quality Assessment (LDOPE) team during the initial burn maneuver, the drift period, and the second burn maneuver. A detailed summary of the rephasing maneuver prepared by the NASA's VCST Geometric Calibration Group can be found here.

Several granules were affected during the drift period and the Geolocation team observed an increase in the track direction error by ~35m during the second propulsive burn on April 4th, 2024. The track direction error shows a sudden increase of ~400m after the second burn on April 4th, 2024, that has been investigated by the geolocation team.
J1 Track/Scan Shift plot

The NOAA-20 scan-to-scan maximum underlap after the first burn was found to be ~250m in ascending mode, at 15 degrees from nadir and may have introduced small underlap related gaps. The L2Gs were inspected throughout the rephasing period for any potential underlap between scans that may be visible as "black" strip in the east-west direction in the tropical region, and no gaps were found. Extended granules after both the burn periods were evaluated for any potential geolocation artifacts and additional impacted granules were identified after the second propulsive burn and were noted. The below listed granules are impacted during the rephasing maneuver and the data is not recoverable.

* Initial Burn 3/20/24 (2024/080) 17:06-17:42 (inclusive)
* Invalid Post-Maneuver TLE 3/21/24 (2024/081) 17:30 - 18:00 (inclusive)
* Second Burn 4/04/24 (2024/095) 11:48 - 13:12 (inclusive)

The images below from 2024/086 and 2024/097 shows the land surface reflectance, land surface temperature, and day-time fire during and after the rephasing period respectively.




Global Browse Image
VJ109-Band I1, I2, and I1
Day A2024/086 (2024-03-27), AS2200
Global Browse Image
VJ121 - LST/Daytime
A2024086 (2024-03-27), AS2200
Global Browse Image
VJ114-Fire/Daytime
Day A2024/086 (2024-03-27), AS2200

Global Browse Image
VJ109-Band I1, I2, and I1
Day A2024/097 (2024-04-08), AS2200
Global Browse Image
VJ121 - LST/Daytime
A2024097 (2024-04-08), AS2200
Global Browse Image
VJ114-Fire/Daytime
Day A2024/097 (2024-04-08), AS2200


Occurrence:
PGE:
Case Name: HC_N20_L1B_24101
Loading...