All,
The apogee contact was nominal. The inertial maneuver was successful.
Tasks Accomplished:
Reset FDC Totals
Results from the Inertial Maneuver:
Q1 -0.65827700 ActNor.EstInrToBdy[0]
Q2 -0.18105500 ActNor.EstInrToBdy[1]
Q3 0.66707700 ActNor.EstInrToBdy[2]
Q4 0.29816000 ActNor.EstInrToBdy[3]
GPS sec 1378940513 ActNor.EstTime
UTC time
09/16/2023 23:01:39 output
MPS Diff
0.750 deg
MPS Cmd Vector X -0.98701100
MPS Cmd Vector Y 0.151052000
MPS Cmd Vector Z 0.054706000
CSS Angle TLM 0.484164
CSS Sun-Pointing Angle 0.968328
12 Sept 23@16:00:00
CSS Angle TLM 0.227087
CSS Sun-Pointing Angle 0.454174
16 Sept 23@23:00:00
Pre-Burn
Thruster 1 11552 12 Sept 23@16:00:00
Thruster 2 11280
Thruster 3 13792
Thruster 4 14064
Post-Burn
Thruster 1 11842 16 Sept 23@23:00:00
Thruster 2 11552
Thruster 3 14096
Thruster 4 14368
Number of Pulses
Thruster 1 290
Thruster 2 272
Thruster 3 304
Thruster 4 304
Thruster Pairs
Thruster 1 & 2 562
Thruster 3 & 4 608
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
Office (703) 406-5976
Cell (301) 606-1430