All,
The apogee contact was nominal and the inertial maneuver was successful.
Results from the inertial maneuver:
Q1 0.11554000 ActNor.EstInrToBdy[0]
Q2 -0.57226100 ActNor.EstInrToBdy[1]
Q3 -0.71752000 ActNor.EstInrToBdy[2]
Q4 0.37991100 ActNor.EstInrToBdy[3]
GPS sec 1375002039 ActNor.EstTime
UTC time
08/02/2023 09:00:25 output
MPS Diff
0.744 deg
MPS Cmd Vector X –0.606906000
MPS Cmd Vector Y 0.733076000
MPS Cmd Vector Z 0.307024000
CSS Angle TLM 0.306467
CSS Sun-Pointing Angle 0.612934
24 July 23@08:00:00
CSS Angle TLM 0.49456
CSS Sun-Pointing Angle 0.98912
24 July 23@08:00:00
Pre-Burn
Thruster 1 8832 24 July 23@08:00:00
Thruster 2 8624
Thruster 3 10880
Thruster 4 11088
Post-Burn
Thruster 1 9088 02 Aug 23@09:00:00
Thruster 2 8880
Thruster 3 11168
Thruster 4 11376
Number of Pulses
Thruster 1 256
Thruster 2 256
Thruster 3 288
Thruster 4 288
Thruster Pairs
Thruster 1 & 2 512
Thruster 3 & 4 576
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
Office (703) 406-5976
Cell (301) 606-1430