All,
The apogee contact was nominal, and the inertial maneuver was successful.
Results from the Inertial Maneuver:
Q1 -0.23013400 ActNor.EstInrToBdy[0]
Q2 -0.49981700 ActNor.EstInrToBdy[1]
Q3 -0.79537100 ActNor.EstInrToBdy[2]
Q4 0.25417800 ActNor.EstInrToBdy[3]
GPS sec 1371038452 ActNor.EstTime
UTC time
06/17/2023 12:00:38 output
MPS Diff
0.537 deg
MPS Cmd Vector X 0.109502000
MPS Cmd Vector Y 0.915867000
MPS Cmd Vector Z 0.386260000
CSS Angle TLM 0.193827
CSS Sun-Pointing Angle 0.387654
13 May 23@03:00:00
CSS Angle TLM 0.4673
CSS Sun-Pointing Angle 0.9346
17 May 23@12:00:00
Pre-Burn
Thruster 1 6096 13 May 23@03:00:00
Thruster 2 5952
Thruster 3 7872
Thruster 4 8016
Post-Burn
Thruster 1 6368 17 May 23@12:00:00
Thruster 2 6224
Thruster 3 8208
Thruster 4 8352
Number of Pulses
Thruster 1 272
Thruster 2 272
Thruster 3 336
Thruster 4 336
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 672
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
Office (703) 406-5976
Cell (301) 606-1430