[Isocops] IBEX Goat Herder 8 Oct 2020

[Perry, Timothy E [US] (IS)]

All,
    The apogee contact was nominal for CMD & TLM. The inertial maneuver was successful. The Orbit #504 Battery Balancing ATS and Hi High Gain Cal ATS was uplinked.

Tasks Accomplished:
CAR # 1123 ATS Upload
   IBEX_2020_287_o0504a_HGC_V001 64 Cmds
CAR # 1124 ATS Upload
   IBEX_2020_287_o0504a_Bat_Bal_V001 2 Cmds

Results from the Inertial maneuver:
Q1 0.65931100 ActNor.EstInrToBdy[0]
Q2 -0.33438500 ActNor.EstInrToBdy[1]
Q3 -0.52140800 ActNor.EstInrToBdy[2]
Q4 0.42618100 ActNor.EstInrToBdy[3]

GPS sec 1286236344 ActNor.EstTime

UTC time 10/08/2020 23:52:10 output
MPS Cmd Vector X -0.973015000
MPS Cmd Vector Y -0.207513000
MPS Cmd Vector Z -0.100900000
MPS Diff 0.558 deg
CSS Angle TLM 1.63327
CSS Sun-Pointing Angle 3.26654
  04 Oct 20 @ 08:00:00
CSS Angle TLM 0.0791294
CSS Sun-Pointing Angle 0.1582588
  08 Oct 20 @ 23:30:00
Pre-Burn
Thruster 1 5264 04 Oct 20 @ 08:00:00
Thruster 2 5136
Thruster 3 6240
Thruster 4 6368
Post-Burn   `
Thruster 1 5408 08 Oct 20 @ 23:30:00
Thruster 2 5280
Thruster 3 6432
Thruster 4 6560
Number of Pulses
Thruster 1 144
Thruster 2 144
Thruster 3 192
Thruster 4 192
Thruster Pairs
Thruster 1 & 2 288
Thruster 3 & 4 384



Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
timothy.perry at ngc.com
Office (703) 406-5976
Cell (301) 606-1430

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