[Isocops] IBEX Goat Herder for 16 March 2024

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

All,
   The spacecraft is nominal. The inertial maneuver was successful.

Results from the Inertial Maneuver:
Q1 -0.29876700 ActNor.EstInrToBdy[0]
Q2 0.64758800 ActNor.EstInrToBdy[1]
Q3 -0.32093500 ActNor.EstInrToBdy[2]
Q4 0.62319200 ActNor.EstInrToBdy[3]

GPS sec 1394629516 ActNor.EstTime
UTC time 03/16/2024 13:05:02 output

MPS Diff 0.648 deg

MPS Cmd Vector X 0.99906300
MPS Cmd Vector Y -0.035202000
MPS Cmd Vector Z -0.025182000

CSS Angle TLM 1.34988
CSS Sun-Pointing Angle 2.69976
  12 Mar 24 @11:00:00

CSS Angle TLM 0.974179
CSS Sun-Pointing Angle 1.948358
  16 Mar 24 @13:00:00

Pre-Burn
Thruster 1 21056 12 Mar 24 @11:00:00
Thruster 2 20400
Thruster 3 28448
Thruster 4 29104

Post-Burn
Thruster 1 21344 16 Mar 24 @13:00:00
Thruster 2 20688
Thruster 3 28752
Thruster 4 29408
Number of Pulses
Thruster 1 288
Thruster 2 288
Thruster 3 304
Thruster 4 304
Thruster Pairs
Thruster 1 & 2 576
Thruster 3 & 4 608



Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
timothy.perry at ngc.com<mailto:timothy.perry at ngc.com>
Office (703) 406-5976
IBEX MOC (703)404-7470
Cell (301) 606-1430

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