[Isocops] IBEX Goat Herder for 6 March 2022

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

All,
    The perigee contacts were nominal for CMD and TLM. The inertial maneuver was successful. The 18 day timer was reset. The spacecraft clock was set and orbit 561 ATS was uplinked.
        Tim

Tasks Accomplished:
  Set Spacecraft clock
  Reset 18 Day Timer
  CAR 1230 Orbit #561 ATS upload
  SSR dump -> Dump New
  Reset FDC Totals

Results from the Inertial Maneuver:
Q1 0.62935500 ActNor.EstInrToBdy[0]
Q2 0.38778800 ActNor.EstInrToBdy[1]
Q3 0.48198300 ActNor.EstInrToBdy[2]
Q4 0.47034600 ActNor.EstInrToBdy[3]

GPS sec 1330610440 ActNor.EstTime

UTC time 03/06/2022 14:00:26 output

MPS Diff 0.806 deg

MPS Cmd Vector X 0.973273000
MPS Cmd Vector Y -0.206485000
MPS Cmd Vector Z -0.100518000

CSS Angle TLM 0.861846
CSS Sun-Pointing Angle 1.723692
  02 Mar 22 @ 14:00:00

CSS Angle TLM 0.900296
CSS Sun-Pointing Angle 1.800592
  06 Mar 22 @ 14:00:00

Pre-Burn
Thruster 1 17600 02 Mar 22 @ 14:00:00
Thruster 2 17088
Thruster 3 22304
Thruster 4 22816
Post-Burn
Thruster 1 17872 06 Mar 22 @ 14:00:00
Thruster 2 17360
Thruster 3 22608
Thruster 4 23120
Number of Pulses
Thruster 1 272
Thruster 2 272
Thruster 3 304
Thruster 4 304
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 608


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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