All,
The perigee contacts were nominal. The inertial maneuver was successful. We updated the Hi sweep table from normal to background. The SSR was dumped and the orbit 633 ATS was uplinked.
Tasks Accomplished:
SSR Dump -> Dump New
Reset FDC Totals
Reset Master Timer
CAR # 1335 - 2024 ISN Season and Hi Background sweep test
Completed Pass #2 – Upload Hi Background table
CAR #1362 – Orbit #633 ATS Upload
IBEX_2023_363_o0633a_v001 98 commands
Results from the Inertial maneuver:
Q1 0.80863500 ActNor.EstInrToBdy[0]
Q2 0.20832400 ActNor.EstInrToBdy[1]
Q3 -0.14915900 ActNor.EstInrToBdy[2]
Q4 0.52958700 ActNor.EstInrToBdy[3]
GPS sec 1387080001 ActNor.EstTime
UTC time
12/20/2023 03:59:47 output
MPS Diff
0.794 deg
MPS Cmd Vector X -0.01682000
MPS Cmd Vector Y -0.913355000
MPS Cmd Vector Z -0.406816000
CSS Angle TLM 1.07265
CSS Sun-Pointing Angle 2.1453
15 Dec 23 @21:00:00
CSS Angle TLM 0.762589
CSS Sun-Pointing Angle 1.525178
20 Dec 23 @04:00:00
Pre-Burn
Thruster 1 16288 15 Dec 23 @21:00:00
Thruster 2 15776
Thruster 3 21696
Thruster 4 22208
Post-Burn
Thruster 1 16624 20 Dec 23 @04:00:00
Thruster 2 16112
Thruster 3 22064
Thruster 4 22576
Number of Pulses
Thruster 1 336
Thruster 2 336
Thruster 3 368
Thruster 4 368
Thruster Pairs
Thruster 1 & 2 672
Thruster 3 & 4 736
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
Office (703) 406-5976
Cell (301) 606-1430