All,
The Apogee pass was nominal for CMD and TLM. The Inertial maneuver was successful.
The Orbit 445 ATS was uplinked on this pass.
Results for the inertial maneuver:
Q1 0.30916700 ActNor.EstInrToBdy[0]
Q2 0.55757500 ActNor.EstInrToBdy[1]
Q3 0.62988100 ActNor.EstInrToBdy[2]
Q4 0.44359300 ActNor.EstInrToBdy[3]
GPS sec 1239814947.000 ActNor.EstTime
MPS Diff 0.705 deg
MPS Cmd Vector X 0.882057000
MPS Cmd Vector Y 0.436227000
MPS Cmd Vector Z 0.177995000
CSS Angle TLM 0.350545
CSS Sun-Pointing Angle 0.70109
16 Apr 19 @ 09:00
CSS Angle TLM 0.199851
CSS Sun-Pointing Angle 0.399702
20 Apr 19 @ 17:00
Pre-Burn
Thruster 1 9360 16 Apr 19 @ 09:00
Thruster 2 9136
Thruster 3 11488
Thruster 4 11712
Post-Burn
Thruster 1 9632 20 Apr 19 @ 17:00
Thruster 2 9408
Thruster 3 11792
Thruster 4 12016
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
tim.perry@orbitalatk.com
Office (703) 406-5976
Cell (301) 606-1430
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