The apogee contact for Orbit #413 was nominal for command/telemetry. The inertial maneuver was successful.
Q1 -0.55712100 ActNor.EstInrToBdy[0]
Q2 -0.03213440 ActNor.EstInrToBdy[1]
Q3 0.23141900 ActNor.EstInrToBdy[2]
Q4 0.79688700 ActNor.EstInrToBdy[3]
GPS sec 1215521993.000 ActNor.EstTime
UTC time
07/13/2018 12:59:39 output
MPS Diff
0.552
MPS Cmd Vector X
-0.312009000
MPS Cmd Vector Y
0.875739000
MPS Cmd Vector Z
0.368417000
CSS Angle TLM 0.476423
CSS Sun-Pointing Angle 0.952846
9 July 18 @0030
CSS Angle TLM 0.799663
CSS Sun-Pointing Angle 1.599326
13 July 18 @1300
Pre-Burn
Thruster 1 1408 9 July 18 @0030
Thruster 2 1376
Thruster 3 1504
Thruster 4 1536
Post-Burn
Thruster 1 1664 13 July 18 @1300
Thruster 2 1632
Thruster 3 1792
Thruster 4 1824
Number of Pulses
Thruster 1 256
Thruster 2 256
Thruster 3 288
Thruster 4 288
Thruster Pairs
Thruster 1 & 2 512
Thruster 3 & 4 576
Eric Chubin
Mission Operations Engineer - OCO2, IBEX
Northrop Grumman Innovation Systems
OCO2 MOC#: (703) 429 - 7015
Mobile#: (240) 328 - 2098
Eric.Chubin@ngc.com
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