All,
The apogee contact was nominal. The inertial maneuver was successful.
Results from the Inertial Maneuver:
Q1 -0.30801400 ActNor.EstInrToBdy[0]
Q2 0.55234200 ActNor.EstInrToBdy[1]
Q3 -0.01634920 ActNor.EstInrToBdy[2]
Q4 0.77445300 ActNor.EstInrToBdy[3]
GPS sec 1366297188 ActNor.EstTime
UTC time
04/23/2023 14:59:34 output
MPS Diff
0.644 deg
MPS Cmd Vector X 0.864340000
MPS Cmd Vector Y 0.465283000
MPS Cmd Vector Z 0.190860000
CSS Angle TLM 0.880934
CSS Sun-Pointing Angle 1.761868
18 Apr 23@06:30:00
CSS Angle TLM 0.990908
CSS Sun-Pointing Angle 1.981816
23 Apr 23@15:00:00
Pre-Burn
Thruster 1 2944 18 Apr 23@06:30:00
Thruster 2 2864
Thruster 3 4272
Thruster 4 4352
Post-Burn
Thruster 1 3120 23 Apr 23@15:00:00
Thruster 2 3040
Thruster 3 4480
Thruster 4 4560
Number of Pulses
Thruster 1 176
Thruster 2 176
Thruster 3 208
Thruster 4 208
Thruster Pairs
Thruster 1 & 2 352
Thruster 3 & 4 416
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
Office (703) 406-5976
Cell (301) 606-1430
