All,
The perigee contacts were nominal. The inertial maneuver was successful. We changed the Hi sweep table back to normal from background sweep. The Orbit 594 ats was uplinked
and the SSR was dumped.
Tasks Accomplished:
CAR #1269 2023 ISN Season and Hi Background Sweep Table uplink
Completed Pass# 3 Hi Normal Sweep Table upload
CAR #11286 Orbit 594 ATS upload
IBEX_2023_009_o0594a_v001 98 Commands
SSR Dump -> Dump New
Set Spacecraft clock
Reset Master Reset Timer
Reset FDC totals
Results from the Inertial Maneuver:
Q1 0.73212500 ActNor.EstInrToBdy[0]
Q2 -0.40025500 ActNor.EstInrToBdy[1]
Q3 0.35593000 ActNor.EstInrToBdy[2]
Q4 0.42083600 ActNor.EstInrToBdy[3]
GPS sec 1356514278 ActNor.EstTime
UTC time
12/31/2022 09:31:04 output
MPS Diff
0.540 deg
MPS Cmd Vector X 0.188365000
MPS Cmd Vector Y -0.897036000
MPS Cmd Vector Z -0.399805000
CSS Angle TLM 0.986753
CSS Sun-Pointing Angle 1.973506
27 Dec 22@18:00:00
CSS Angle TLM 0.589835
CSS Sun-Pointing Angle 1.17967
31 Dec 22@09:30:00
Pre-Burn
Thruster 1 2656 27 Dec 22@18:00:00
Thruster 2 2576
Thruster 3 3776
Thruster 4 3856
Post-Burn
Thruster 1 2912 31 Dec 22@09:30:00
Thruster 2 2832
Thruster 3 4080
Thruster 4 4160
Number of Pulses
Thruster 1 256
Thruster 2 256
Thruster 3 304
Thruster 4 304
Thruster Pairs
Thruster 1 & 2 512
Thruster 3 & 4 608
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
Office (703) 406-5976
Cell (301) 606-1430