[Isocops] IBEX Goat Herder for 11th & 12th of March 2024

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

All,
   The perigee contacts were nominal. The inertial maneuver was successful. The orbit 642 ATS was uplinked. We did drop 1 command during the uplink. The command was later re-uplinked. The SSR was successfully dumped with zero errors.

Tasks Accomplished:
SSR Dump -> Dump New
Reset FDC Totals
CAR# 1381 Orbit# 642 ATS Upload
Set the Spacecraft Clock
Reset Master Timer

Results from the Inertial Maneuver:
Q1 0.06286580 ActNor.EstInrToBdy[0]
Q2 0.72170500 ActNor.EstInrToBdy[1]
Q3 -0.02132680 ActNor.EstInrToBdy[2]
Q4 0.68901000 ActNor.EstInrToBdy[3]

GPS sec 1394276531 ActNor.EstTime
UTC time 03/12/2024 11:01:57 output

MPS Diff 0.657 deg

MPS Cmd Vector X 0.99213300
MPS Cmd Vector Y -0.110514000
MPS Cmd Vector Z -0.058819000

CSS Angle TLM 1.12106
CSS Sun-Pointing Angle 2.24212
  07 Mar 24 @17:00:00

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

Pre-Burn
Thruster 1 20784 07 Mar 24 @17:00:00
Thruster 2 20128
Thruster 3 28160
Thruster 4 28816
Post-Burn
Thruster 1 21056 12 Mar 24 @11:00:00
Thruster 2 20400
Thruster 3 28448
Thruster 4 29104
Number of Pulses
Thruster 1 272
Thruster 2 272
Thruster 3 288
Thruster 4 288
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 576



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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