All,
The spacecraft is nominal. The perigee inertial maneuver was successful. Both orbit’s 660 and 661 ats was uplinked. The SSR was dumped with zero errors.
The second contact was used for monitoring SOH. The AGC was low and not a good pass for commanding.
Tasks Accomplished:
SSR Dump -> Dump_New
Reset Master Timer
Reset FDC Totals
CAR #1411 Orbit# 660 ATS Upload
IBEX_2024_244_o0660a_V002 98 cmds
CAR #1409 Orbit# 661 ATS Upload
IBEX_2024_253_o0661a_V001 96 cmds
Results from the Inertial Maneuver:
Q1 0.30170100 ActNor.EstInrToBdy[0]
Q2 -0.56919700 ActNor.EstInrToBdy[1]
Q3 -0.59503500 ActNor.EstInrToBdy[2]
Q4 0.48054700 ActNor.EstInrToBdy[3]
GPS sec 1409087092 ActNor.EstTime
UTC time
08/30/2024 21:04:38 output
MPS Diff
0.733 deg
MPS Cmd Vector X -0.90894100
MPS Cmd Vector Y 0.38601000
MPS Cmd Vector Z 0.15755500
CSS Angle TLM 0.349246
CSS Sun-Pointing Angle 0.698492
25 Aug 24 @23:30:00
CSS Angle TLM 0.338041
CSS Sun-Pointing Angle 0.676082
30 Aug 24 @21:00:00
Pre-Burn
Thruster 1 4672 25 Aug 24 @23:30:00
Thruster 2 4576
Thruster 3 4880
Thruster 4 4976
Post-Burn
Thruster 1 4944 30 Aug 24 @21:00:00
Thruster 2 4848
Thruster 3 5184
Thruster 4 5280
Number of Pulses
Thruster 1 272
Thruster 2 272
Thruster 3 304
Thruster 4 304
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 608
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
Office (703) 406-5976
IBEX MOC (703)404-7470
Cell (301) 606-1430