All,
The apogee contact was nominal, and the inertial maneuver was successful.
Tasks Accomplished:
Reset FDC Totals
Results from the Inertial Maneuver:
Q1 -0.48950900 ActNor.EstInrToBdy[0]
Q2 0.33651500 ActNor.EstInrToBdy[1]
Q3 -0.14065200 ActNor.EstInrToBdy[2]
Q4 0.79205800 ActNor.EstInrToBdy[3]
GPS sec 1367845519 ActNor.EstTime
UTC time
05/11/2023 13:05:05 output
MPS Diff
0.578 deg
MPS Cmd Vector X 0.667656000
MPS Cmd Vector Y 0.686949000
MPS Cmd Vector Z 0.286943000
CSS Angle TLM 0.291412
CSS Sun-Pointing Angle 0.582824
07 May 23@12:00:00
CSS Angle TLM 0.333378
CSS Sun-Pointing Angle 0.666756
11 May 23@13:00:00
Pre-Burn
Thruster 1 3968 07 May 23@12:00:00
Thruster 2 3888
Thruster 3 5408
Thruster 4 5488
Post-Burn
Thruster 1 4224 11 May 23@13:00:00
Thruster 2 4144
Thruster 3 5680
Thruster 4 5760
Number of Pulses
Thruster 1 256
Thruster 2 256
Thruster 3 272
Thruster 4 272
Thruster Pairs
Thruster 1 & 2 512
Thruster 3 & 4 544
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
Office (703) 406-5976
Cell (301) 606-1430