[Isocops] IBEX Goat Herder for 17 Nov 2019

[Chubin, Eric [US] (IS)]

All,

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

The following was accomplished during the pass:
Set Static Z Rate from 4.174 to 4.182
Back-Orbit Buffer Downlink

Results from the Sun Maneuver:

CSS Angle TLM   0.855237
CSS Sun-Pointing Angle   1.710474
                              10 Nov 19 @ 06:00
CSS Angle TLM   0.666466
CSS Sun-Pointing Angle   1.332932
                              17 Nov 19 @ 00:30
Pre-Burn
Thruster 1 20352 10 Nov 19 @ 06:00
Thruster 2 19728
Thruster 3 26448
Thruster 4 27072
Post-Burn
Thruster 1 20656 17 Nov 19 @ 00:30
Thruster 2 20032
Thruster 3 27008
Thruster 4 27632
Number of Pulses
Thruster 1 304
Thruster 2 304
Thruster 3 560
Thruster 4 560
Thruster Pairs
Thruster 1 & 2    608
Thruster 3 & 4    1120

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

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