[Isocops] IBEX Goat Herder 23 May 2021

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

All,

   The apogee contact was nominal for CMD & TLM. The inertial maneuver was successful.



Results from the Inertial Maneuver:
Q1 -0.27806300 ActNor.EstInrToBdy[0]
Q2 0.49911500 ActNor.EstInrToBdy[1]
Q3 0.39280900 ActNor.EstInrToBdy[2]
Q4 0.72060100 ActNor.EstInrToBdy[3]

GPS sec 1305810008 ActNor.EstTime

UTC time 05/23/2021 12:59:54 output

MPS Cmd Vector X 0.496176000
MPS Cmd Vector Y 0.800531000
MPS Cmd Vector Z 0.336093000

MPS Diff 0.818 deg

CSS Angle TLM 0.586842
CSS Sun-Pointing Angle 1.173684
  19 May 21 @ 15:00:00

CSS Angle TLM 0.297393
CSS Sun-Pointing Angle 0.594786
  23 May 21 @ 13:00:00

Pre-Burn
Thruster 1 1408 19 May 21 @ 15:00:00
Thruster 2 1376
Thruster 3 1520
Thruster 4 1552

Post-Burn
Thruster 1 1680 23 May 21 @ 13:00:00
Thruster 2 1648
Thruster 3 1792
Thruster 4 1824

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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