[Isocops] Goat Herder for 4 Oct 2018

[Chubin, Eric]

All,

The Apogee pass was nominal for CMD and TLM. The Inertial maneuver was successful.

Q1          -0.45593300        ActNor.EstInrToBdy[0]
Q2          -0.56338800        ActNor.EstInrToBdy[1]
Q3          0.49161700          ActNor.EstInrToBdy[2]
Q4          0.48273400          ActNor.EstInrToBdy[3]
GPS sec                1222678921.000 ActNor.EstTime
MPS Cmd Vector X          -0.991748000
MPS Cmd Vector Y          -0.113171000
MPS Cmd Vector Z          -0.060230000
MPS Diff              0.557
CSS Angle TLM  0.333965
CSS Sun-Pointing Angle 0.66793
                                28 Sept 18 @ 12:30
CSS Angle TLM  0.958792
CSS Sun-Pointing Angle 1.917584
                                4  Oct 18 @ 09:00
Pre-Burn
Thruster 1           6384       28 Sept 18 @ 12:30
Thruster 2           6224
Thruster 3           6848
Thruster 4           7008
Post-Burn
Thruster 1           6656       4  Oct 18 @ 09:00
Thruster 2           6496
Thruster 3           7152
Thruster 4           7312
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

Eric Chubin
Mission Operations Engineer - OCO2, IBEX
Northrop Grumman Innovation Systems
OCO2 MOC#: (703) 429 - 7015
Mobile#: (240) 328 - 2098
Eric.Chubin at ngc.com<mailto:Eric.Chubin at ngc.com>


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