All,
The Apogee pass was nominal for CMD and TLM. The Inertial maneuver was successful.
Q1 -0.49889600 ActNor.EstInrToBdy[0]
Q2 0.29871200 ActNor.EstInrToBdy[1]
Q3 -0.09514790 ActNor.EstInrToBdy[2]
Q4 0.80797300 ActNor.EstInrToBdy[3]
MPS Cmd Vector X 0.577243000
MPS Cmd Vector Y 0.753202000
MPS Cmd Vector Z 0.315401000
GPS sec
1242216137.000 ActNor.EstTime
MPS Diff
0.526 deg
CSS Angle TLM
0.609093
CSS Sun-Pointing Angle
1.218186
13 May 19 @ 19:00
CSS Angle TLM
0.3499986
CSS Sun-Pointing Angle
0.6999972
18 May 19 @ 12:00
Pre-Burn
Thruster 1
11008 13 May 19 @ 19:00
Thruster 2
10752
Thruster 3
13296
Thruster 4
13552
Post-Burn
Thruster 1
11312 18 May 19 @ 12:00
Thruster 2
11024
Thruster 3
13600
Thruster 4
13888
Number of Pulses
Thruster 1
304
Thruster 2
272
Thruster 3
304
Thruster 4
336
Thruster Pairs
Thruster 1 & 2
576
Thruster 3 & 4
640
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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