All,
The apogee contact was nominal. The inertial maneuver was successful.
Results from the Inertial Maneuver
Q1 0.66499700 ActNor.EstInrToBdy[0]
Q2 -0.50643400 ActNor.EstInrToBdy[1]
Q3 0.38201700 ActNor.EstInrToBdy[2]
Q4 0.39416500 ActNor.EstInrToBdy[3]
GPS sec 1356199394 ActNor.EstTime
UTC time
12/27/2022 18:03:00 output
MPS Diff
0.400 deg
MPS Cmd Vector X 0.109580000
MPS Cmd Vector Y -0.908310000
MPS Cmd Vector Z -0.403689000
CSS Angle TLM 0.669688
CSS Sun-Pointing Angle 1.339376
22 Dec 22@12:00:00
CSS Angle TLM 0.986753
CSS Sun-Pointing Angle 1.973506
27 Dec 22@18:00:00
Pre-Burn
Thruster 1 2352 22 Dec 22@12:00:00
Thruster 2 2304
Thruster 3 3440
Thruster 4 3488
Post-Burn
Thruster 1 2656 27 Dec 22@18:00:00
Thruster 2 2576
Thruster 3 3776
Thruster 4 3856
Number of Pulses
Thruster 1 304
Thruster 2 272
Thruster 3 336
Thruster 4 368
Thruster Pairs
Thruster 1 & 2 576
Thruster 3 & 4 704
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
Office (703) 406-5976
Cell (301) 606-1430