[Isocops] IBEX Goat Herder for 24 May 2020

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

All,
   The apogee pass was nominal for CMD and TLM. The inertial maneuver was successful. We did have another star tracker reset. I executed CAR 344 to clear all errors. The tracker recovered nominally and was at 80% during the contact. The BUS ATS for orbit 491 was uplinked and the current command count is at 216.

TASKS accomplished:
CAR 344 - Reset FDC Totals and Response latch values
CAR 2000 - ATS upload - IBEX_2020_167_o0491a_BUS_V001 48 cmds


Results from the inertial maneuver:
Q1 -0.53407900 ActNor.EstInrToBdy[0]
Q2 -0.20434900 ActNor.EstInrToBdy[1]
Q3 -0.65140300 ActNor.EstInrToBdy[2]
Q4 0.49867300 ActNor.EstInrToBdy[3]
GPS sec 1274357266 ActNor.EstTime
UTC time 05/24/2020 12:07:32 output
MPS Diff 0.641 deg
MPS Cmd Vector X 0.487235000
MPS Cmd Vector Y 0.805187000
MPS Cmd Vector Z 0.338048000
CSS Angle TLM 0.745723
CSS Sun-Pointing Angle 1.491446
  19 May 20 @23:30
CSS Angle TLM 0.5203
CSS Sun-Pointing Angle 1.0406
  24 May 20 @12:00
Pre-Burn
Thruster 1 9440 19 May 20 @23:30
Thruster 2 9168
Thruster 3 12064
Thruster 4 12336
Post-Burn
Thruster 1 9712 24 May 20 @12:00
Thruster 2 9440
Thruster 3 12352
Thruster 4 12624
Number of Pulses
Thruster 1 272
Thruster 2 272
Thruster 3 288
Thruster 4 288
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 576



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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