All,
The apogee contact was nominal, and the inertial maneuver was successful.
Tasks Accomplished:
Reset FDC Totals
Results from the Inertial Maneuver:
Q1 -0.25988300 ActNor.EstInrToBdy[0]
Q2 -0.50120100 ActNor.EstInrToBdy[1]
Q3 -0.82524500 ActNor.EstInrToBdy[2]
Q4 0.01511730 ActNor.EstInrToBdy[3]
GPS sec 1369483265 ActNor.EstTime
UTC time
05/30/2023 12:00:51 output
MPS Diff
0.775 deg
MPS Cmd Vector X 0.405835000
MPS Cmd Vector Y 0.842434000
MPS Cmd Vector Z 0.354405000
CSS Angle TLM 0.0279765
CSS Sun-Pointing Angle 0.055953
25 May 23@17:00:00
CSS Angle TLM 0.237388
CSS Sun-Pointing Angle 0.474776
30 May 23@12:00:00
Pre-Burn
Thruster 1 5104 25 May 23@17:00:00
Thruster 2 4992
Thruster 3 6592
Thruster 4 6704
Post-Burn
Thruster 1 5376 30 May 23@12:00:00
Thruster 2 5264
Thruster 3 6880
Thruster 4 6992
Number of Pulses
Thruster 1 272
Thruster 2 272
Thruster 3 288
Thruster 4 288
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 576
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
Office (703) 406-5976
Cell (301) 606-1430