All,
The apogee contact was nominal. The inertial maneuver was successful.
Results from the Inertial Maneuver:
Q1 -0.41544700 ActNor.EstInrToBdy[0]
Q2 -0.57452100 ActNor.EstInrToBdy[1]
Q3 0.41999400 ActNor.EstInrToBdy[2]
Q4 0.56651100 ActNor.EstInrToBdy[3]
GPS sec 1348268443 ActNor.EstTime
UTC time
09/26/2022 23:00:29 output
MPS Diff
0.560 deg
MPS Cmd Vector X -0.999868000
MPS Cmd Vector Y -0.007818000
MPS Cmd Vector Z -0.014276000
CSS Angle TLM 0.251788
CSS Sun-Pointing Angle 0.503576
22 Sept 22 @02:00:00
CSS Angle TLM 0.23239
CSS Sun-Pointing Angle 0.46478
26 Sept 22 @23:00:00
Pre-Burn
Thruster 1 6192 22 Sept 22 @02:00:00
Thruster 2 6032
Thruster 3 7344
Thruster 4 7504
Post-Burn
Thruster 1 6480 26 Sept 22 @23:00:00
Thruster 2 6320
Thruster 3 7664
Thruster 4 7824
Number of Pulses
Thruster 1 288
Thruster 2 288
Thruster 3 320
Thruster 4 320
Thruster Pairs
Thruster 1 & 2 576
Thruster 3 & 4 640
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
Office (703) 406-5976
Cell (301) 606-1430