[Isocops] IBEX Goat Herder for 9 April 2020

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

All,
    The apogee contacts was nominal for CMD and TLM. The inertial maneuver was successful. the contact was taken on string 1.

Results from the Inertial maneuver:
Q1 -0.18837900 ActNor.EstInrToBdy[0]
Q2 0.63514400 ActNor.EstInrToBdy[1]
Q3 -0.00190548 ActNor.EstInrToBdy[2]
Q4 0.74908700 ActNor.EstInrToBdy[3]
GPS sec 1270472518 ActNor.EstTime
MPS Diff 0.629 deg
MPS Cmd Vector X 0.952508000
MPS Cmd Vector Y 0.283249000
MPS Cmd Vector Z 0.111798000
CSS Angle TLM 0.260196
CSS Sun-Pointing Angle 0.520392
  5 Apr 20 @ 4:30
CSS Angle TLM 0.0625
CSS Sun-Pointing Angle 0.125
  9 Apr 20 @ 13:00
Pre-Burn
Thruster 1 6848 5 Apr 20 @ 4:30
Thruster 2 6656
Thruster 3 9056
Thruster 4 9248
Post-Burn
Thruster 1 7120 9 Apr 20 @ 13:00
Thruster 2 6928
Thruster 3 9376
Thruster 4 9568
Number of Pulses
Thruster 1 272
Thruster 2 272
Thruster 3 320
Thruster 4 320
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 640



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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