[Isocops] IBEX Goat Herder for 26 Feb 2020

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

All,
    The apogee pass was nominal for CMD and TLM. The inertial maneuver was successful.

Results from the Inertial maneuver:
Q1 0.69214000 ActNor.EstInrToBdy[0]
Q2 0.31649200 ActNor.EstInrToBdy[1]
Q3 0.44348100 ActNor.EstInrToBdy[2]
Q4 0.47339200 ActNor.EstInrToBdy[3]
MPS Cmd Vector X 0.916446000
MPS Cmd Vector Y -0.363402000
MPS Cmd Vector Z -0.167526000
GPS sec 1266775195 ActNor.EstTime
UTC time 02/26/2020 17:59:41 output
MPS Diff 0.843 deg
CSS Angle TLM 0.589171
CSS Sun-Pointing Angle 1.178342
  19 Feb 20 @ 23:30
CSS Angle TLM 0.625263
CSS Sun-Pointing Angle 1.250526
  26 Feb 20 @ 18:00
Pre-Burn
Thruster 1 4528 19 Feb 20 @ 23:30
Thruster 2 4384
Thruster 3 6096
Thruster 4 6240
Post-Burn
Thruster 1 4768 26 Feb 20 @ 18:00
Thruster 2 4624
Thruster 3 6384
Thruster 4 6528
Number of Pulses
Thruster 1 240
Thruster 2 240
Thruster 3 288
Thruster 4 288
Thruster Pairs
Thruster 1 & 2 480
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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