All,
The Apogee support was nominal for CMD and TLM. The Inertial maneuver was successful.
Tim
Result from the Inertial maneuver:
Q1 -0.04410930
Q2 0.77754700
Q3 -0.34929300
Q4 0.52102700
GPS sec
1234373667.000
UTC time
02/16/2019 17:34:13
MPS Diff
0.679 deg
MPS Cmd Vector X 0.842234000
MPS Cmd Vector Y -0.490861000
MPS Cmd Vector Z -0.222927000
CSS Angle TLM 1.80353
CSS Sun-Pointing Angle 3.60706
10 Feb 19 @12:00
CSS Angle TLM 0.870207
CSS Sun-Pointing Angle 1.740414
16 Feb 19 @17:30
Pre-Burn
Thruster 1 5984 10 Feb 19 @12:00
Thruster 2 5840
Thruster 3 7040
Thruster 4 7184
Post-Burn
Thruster 1 6272 16 Feb 19 @17:30
Thruster 2 6128
Thruster 3 7344
Thruster 4 7488
Number of Pulses
Thruster 1 288
Thruster 2 288
Thruster 3 304
Thruster 4 304
Thruster Pairs
Thruster 1 & 2 576
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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