All,
The spacecraft is nominal, and the inertial maneuver was successful.
Results from the Inertial Maneuver:
Q1 -0.47685200 ActNor.EstInrToBdy[0]
Q2 -0.42647900 ActNor.EstInrToBdy[1]
Q3 0.30211800 ActNor.EstInrToBdy[2]
Q4 0.70671900 ActNor.EstInrToBdy[3]
GPS sec 1377327668 ActNor.EstTime
UTC time
08/29/2023 07:00:54 output
MPS Diff
0.706 deg
MPS Cmd Vector X -0.89360900
MPS Cmd Vector Y 0.415653000
MPS Cmd Vector Z 0.169401000
CSS Angle TLM 0.0906541
CSS Sun-Pointing Angle 0.1813082
24 Aug 23@22:00:00
CSS Angle TLM 0.32145
CSS Sun-Pointing Angle 0.6429
29 Aug 23@03:00:00
Pre-Burn
Thruster 1 10432 24 Aug 23@22:00:00
Thruster 2 10192
Thruster 3 12640
Thruster 4 12880
Post-Burn
Thruster 1 10704 29 Aug 23@03:00:00
Thruster 2 10464
Thruster 3 12912
Thruster 4 13152
Number of Pulses
Thruster 1 272
Thruster 2 272
Thruster 3 272
Thruster 4 272
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 544
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
Office (703) 406-5976
Cell (301) 606-1430