[Isocops] IBEX Goat Herder for September 24 & 25, 2020

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

All,
    The perigee contacts were nominal for CMD & TLM. The inertial maneuver was successful. The apogee inertial maneuver commands for orbit 502 were deleted and sun maneuver commands were uplinked. The Hi background test was completed. The Instrument commands for orbit #503 were uplinked. The SSR was dumped (Dump New).

Tasks completed:
SSR Dump -> Dump new
CAR #1113 Orbit #501 Hi Background test - Completed
CAR #1120 Upload ATS Orbit #503
    IBEX_2020_278_o0503a_INST_V001 46 CMDS
CAR #1121 Upload ATS Orbit #502
    Delete commands 342 - 355
    IBEX_2020_269_o0502a_Apo_Sun_Man_V001 9 CMDS


Results from the Inertial Maneuver:
Q1 -0.70413100 ActNor.EstInrToBdy[0]
Q2 -0.00142560 ActNor.EstInrToBdy[1]
Q3 0.71002500 ActNor.EstInrToBdy[2]
Q4 0.00786796 ActNor.EstInrToBdy[3]
GPS sec 1285075614 ActNor.EstTime

UTC time 09/25/2020 13:26:40 output
MPS Diff 0.864 deg

MPS Cmd Vector X -0.999951000
MPS Cmd Vector Y 0.007365000
MPS Cmd Vector Z -0.006562000

CSS Angle TLM 0.144018
CSS Sun-Pointing Angle 0.288036
  20 Sept 20 @ 03:00:00

CSS Angle TLM 2.04459
CSS Sun-Pointing Angle 4.08918
  25 Sept 20 @ 12:30:00

Pre-Burn
Thruster 1 4448 20 Sept 20 @ 03:00:00
Thruster 2 4320
Thruster 3 5072
Thruster 4 5200
Post-Burn   `
Thruster 1 4720 25 Sept 20 @ 12:30:00
Thruster 2 4592
Thruster 3 5344
Thruster 4 5472
Number of Pulses
Thruster 1 272
Thruster 2 272
Thruster 3 272
Thruster 4 272
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 544


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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