[Isocops] IBEX Goat Herder for 24 July 23

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

All,
   The apogee contact was nominal. The inertial maneuver was successful. This contact I had to blind acq the spacecraft and send up a transmitter off command. I was able to change the downlink from 2k to 40k. Spacecraft looks nominal.

Tasks Accomplished:
Blind_Acq.scr
STK Off Timed command for 07/24/23 @08:35:00

Results from the Inertial Maneuver:
Q1 0.15229200 ActNor.EstInrToBdy[0]
Q2 -0.54776000 ActNor.EstInrToBdy[1]
Q3 -0.79580900 ActNor.EstInrToBdy[2]
Q4 0.20845500 ActNor.EstInrToBdy[3]

GPS sec 1374220851 ActNor.EstTime

UTC time 07/24/2023 08:00:37 output
MPS Diff 0.994 deg
MPS Cmd Vector X -0.481089000
MPS Cmd Vector Y 0.808220000
MPS Cmd Vector Z 0.339608000
CSS Angle TLM 0.546801
CSS Sun-Pointing Angle 1.093602
  20 July 23 at 08:00:00
CSS Angle TLM 0.769485
CSS Sun-Pointing Angle 1.53897
  24 July 23 at 08:00:00
Pre-Burn
Thruster 1 8304 20 July 23 at 08:00:00
Thruster 2 8096
Thruster 3 10304
Thruster 4 10512
Post-Burn
Thruster 1 8544 24 July 23 at 08:00:00
Thruster 2 8336
Thruster 3 10560
Thruster 4 10768
Number of Pulses
Thruster 1 240
Thruster 2 240
Thruster 3 256
Thruster 4 256
Thruster Pairs
Thruster 1 & 2 480
Thruster 3 & 4 512



Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
timothy.perry at ngc.com<mailto:timothy.perry at ngc.com>
Office (703) 406-5976
Cell (301) 606-1430

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