All,
The spacecraft is nominal and the inertial maneuver was successful.
Results of the Inertial Maneuver:
Q1 -0.57933300 ActNor.EstInrToBdy[0]
Q2 0.15680900 ActNor.EstInrToBdy[1]
Q3 0.71511300 ActNor.EstInrToBdy[2]
Q4 0.35832700 ActNor.EstInrToBdy[3]
GPS sec 1375772440 ActNor.EstTime
UTC time
08/11/2023 07:00:26 output
MPS Diff
0.748 deg
MPS Cmd Vector X -0.719652000
MPS Cmd Vector Y 0.640917000
MPS Cmd Vector Z 0.267070000
CSS Angle TLM 0.231547
CSS Sun-Pointing Angle 0.463094
06 Aug 23@19:00:00
CSS Angle TLM 0.335135
CSS Sun-Pointing Angle 0.67027
11 Aug 23@07:00:00
Pre-Burn
Thruster 1 9392 06 Aug 23@19:00:00
Thruster 2 9152
Thruster 3 11427
Thruster 4 11712
Post-Burn
Thruster 1 9632 11 Aug 23@07:00:00
Thruster 2 9392
Thruster 3 11760
Thruster 4 12000
Number of Pulses
Thruster 1 240
Thruster 2 240
Thruster 3 333
Thruster 4 288
Thruster Pairs
Thruster 1 & 2 480
Thruster 3 & 4 621
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
Office (703) 406-5976
Cell (301) 606-1430