All,
The apogee contact was nominal, and the inertial maneuver was successful.
Tasks Accomplished:
Reset FDC Totals
Results from the Inertial Maneuver:
Q1 -0.43984800 ActNor.EstInrToBdy[0]
Q2 0.33065200 ActNor.EstInrToBdy[1]
Q3 0.62978100 ActNor.EstInrToBdy[2]
Q4 0.54825100 ActNor.EstInrToBdy[3]
GPS sec 1372676647 ActNor.EstTime
UTC time
07/06/2023 11:03:53 output
MPS Diff
4.946 deg
MPS Cmd Vector X -0.195323000
MPS Cmd Vector Y 0.903712000
MPS Cmd Vector Z 0.380990000
CSS Angle TLM 0.712169
CSS Sun-Pointing Angle 1.424338
2 July 23@12:00:00
CSS Angle TLM 0.761818
CSS Sun-Pointing Angle 1.523636
6 July 23@11:00:00
Pre-Burn
Thruster 1 7216 2 July 23@12:00:00
Thruster 2 7040
Thruster 3 9056
Thruster 4 9232
Post-Burn
Thruster 1 7488 6 July 23@11:00:00
Thruster 2 7312
Thruster 3 9360
Thruster 4 9536
Number of Pulses
Thruster 1 272
Thruster 2 272
Thruster 3 304
Thruster 4 304
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 608
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
Office (703) 406-5976
Cell (301) 606-1430