All,
The apogee contact was nominal for CMD & TLM. The Inertial maneuver was successful.
Results from the Inertial Maneuver:
Q1 0.05820200 ActNor.EstInrToBdy[0]
Q2 -0.58571500 ActNor.EstInrToBdy[1]
Q3 -0.65158900 ActNor.EstInrToBdy[2]
Q4 0.47852200 ActNor.EstInrToBdy[3]
GPS sec 1312171293 ActNor.EstTime
UTC time
08/05/2021 04:01:19 output
MPS Diff
0.835 deg
MPS Cmd Vector X -0.644305000
MPS Cmd Vector Y 0.705579000
MPS Cmd Vector Z 0.295008000
CSS Angle TLM 0.611658
CSS Sun-Pointing Angle 1.223316
31 Jul 21 @ 17:00:00
CSS Angle TLM 0.96083
CSS Sun-Pointing Angle 1.92166
05 Aug 21 @ 04:00:00
Pre-Burn
Thruster 1 5696 31 Jul 21 @ 17:00:00
Thruster 2 5568
Thruster 3 6288
Thruster 4 6416
Post-Burn
Thruster 1 5968 05 Aug 21 @ 04:00:00
Thruster 2 5840
Thruster 3 6560
Thruster 4 6688
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
Cell (301) 606-1430