All,
The perigee contacts were nominal. The inertial maneuver was successful. The Orbit 635 ATS was uplinked and the SSR was dumped.
Tasks Accomplished:
Reset FDC Totals
Reset Master Timer
CAR #1364 Orbit 635 ATS uplink
IBEX_2024_016_o0635a_v001 88 commands
SSR Dump -> Dump New
Results From the Inertial Maneuver:
Q1 0.77231200 ActNor.EstInrToBdy[0]
Q2 0.30209500 ActNor.EstInrToBdy[1]
Q3 -0.02475710 ActNor.EstInrToBdy[2]
Q4 0.55826500 ActNor.EstInrToBdy[3]
GPS sec 1388671200 ActNor.EstTime
UTC time
01/07/2024 13:59:46 output
MPS Diff
0.923 deg
MPS Cmd Vector X 0.30587800
MPS Cmd Vector Y -0.869509000
MPS Cmd Vector Z -0.387805000
CSS Angle TLM 0.376385
CSS Sun-Pointing Angle 0.75277
04 Jan 24 @18:00:00
CSS Angle TLM 0.848806
CSS Sun-Pointing Angle 1.697612
07 Jan 24 @14:00:00
Pre-Burn
Thruster 1 17312 04 Jan 24 @18:00:00
Thruster 2 16800
Thruster 3 23008
Thruster 4 23520
Post-Burn
Thruster 1 17680 07 Jan 24 @14:00:00
Thruster 2 17168
Thruster 3 23392
Thruster 4 23904
Number of Pulses
Thruster 1 368
Thruster 2 368
Thruster 3 384
Thruster 4 384
Thruster Pairs
Thruster 1 & 2 736
Thruster 3 & 4 768
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
Office (703) 406-5976
IBEX MOC (703)404-7470
Cell (301) 606-1430