All,
The apogee contact was nominal. The inertial maneuver was successful. I did reset the FDC totals to zero.
Tasks accomplished:
Reset FDC Totals
Results from the Inertial Maneuver:
Q1 -0.44554800 ActNor.EstInrToBdy[0]
Q2 -0.48852300 ActNor.EstInrToBdy[1]
Q3 0.32200700 ActNor.EstInrToBdy[2]
Q4 0.67760100 ActNor.EstInrToBdy[3]
GPS sec 1378101667 ActNor.EstTime
UTC time
09/07/2023 06:00:53 output
MPS Diff
0.703 deg
MPS Cmd Vector X -0.95108900
MPS Cmd Vector Y 0.287223000
MPS Cmd Vector Z 0.113723000
CSS Angle TLM 0.15949
CSS Sun-Pointing Angle 0.31898
02 Sept 23@03:00:00
CSS Angle TLM 0.224684
CSS Sun-Pointing Angle 0.449368
07 Sept 23@07:00:00
Pre-Burn
Thruster 1 11008 02 Sept 23@03:00:00
Thruster 2 10736
Thruster 3 13216
Thruster 4 13488
Post-Burn
Thruster 1 11280 07 Sept 23@07:00:00
Thruster 2 11008
Thruster 3 13488
Thruster 4 13760
Number of Pulses
Thruster 1 272
Thruster 2 272
Thruster 3 272
Thruster 4 272
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 544
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
Office (703) 406-5976
Cell (301) 606-1430