All,
The apogee contact was nominal, and the inertial maneuver was successful.
Tasks Accomplished:
Reset FDC Totals
Results from the Inertial Maneuver:
Q1 -0.61758600 ActNor.EstInrToBdy[0]
Q2 -0.05201660 ActNor.EstInrToBdy[1]
Q3 0.61880600 ActNor.EstInrToBdy[2]
Q4 0.48266100 ActNor.EstInrToBdy[3]
GPS sec 1376618574 ActNor.EstTime
UTC time
08/21/2023 02:02:40 output
MPS Diff
0.665 deg
MPS Cmd Vector X -0.816530000
MPS Cmd Vector Y 0.533529000
MPS Cmd Vector Z 0.220510000
CSS Angle TLM 0.0197823
CSS Sun-Pointing Angle 0.0395646
15 Aug 23@22:00:00
CSS Angle TLM 0.200769
CSS Sun-Pointing Angle 0.401538
21 Aug 23@02:00:00
Pre-Burn
Thruster 1 9904 15 Aug 23@22:00:00
Thruster 2 9664
Thruster 3 12048
Thruster 4 12288
Post-Burn
Thruster 1 10176 21 Aug 23@02:00:00
Thruster 2 9936
Thruster 3 12352
Thruster 4 12592
Number of Pulses
Thruster 1 272
Thruster 2 272
Thruster 3 304
Thruster 4 304
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 608
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
Office (703) 406-5976
Cell (301) 606-1430