[Isocops] IBEX Goat Herder for Jan 4 & 5

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

All,
   The perigee contacts were nominal for CMD and TLM. The Inertial maneuver was successful. The spacecraft looks nominal post eclipse.

Tasks Accomplished:
SSR Dump -> Dump_New & Reset Pointers
CAR 1080 Orbit 474 ATS Upload IBEX_2020_014_o0474a_V001
Reset Master Timer
Reset FDC Totals

Results from the Inertial Maneuver:
Q1 0.66888300 ActNor.EstInrToBdy[0]
Q2 0.49325400 ActNor.EstInrToBdy[1]
Q3 -0.19345000 ActNor.EstInrToBdy[2]
Q4 0.52141400 ActNor.EstInrToBdy[3]
GPS sec 1262232149 ActNor.EstTime
UTC time 01/05/2020 04:02:15 output
MPS Diff 0.782 deg
MPS Cmd Vector X 0.256390000
MPS Cmd Vector Y -0.882730000
MPS Cmd Vector Z -0.393765000
CSS Angle TLM 874469
CSS Sun-Pointing Angle 1748938
  31 Dec 19 @ 19:00
CSS Angle TLM 874469
CSS Sun-Pointing Angle 1748938
  5 Jan 20 @ 04:00
Pre-Burn
Thruster 1 1600 31 Dec 19 @ 19:00
Thruster 2 1552
Thruster 3 2208
Thruster 4 2256
Post-Burn
Thruster 1 1952 5 Jan 20 @ 04:00
Thruster 2 1904
Thruster 3 2592
Thruster 4 2640
Number of Pulses
Thruster 1 352
Thruster 2 352
Thruster 3 384
Thruster 4 384
Thruster Pairs
Thruster 1 & 2 704
Thruster 3 & 4 768



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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