All,
The perigee contacts were nominal. The inertial maneuver was successful. During the first contact we uplinked the Hi Normal Sweep table. The ATS for orbit 644 was uplinked and the SSR was dumped for orbit #642.
Tasks Accomplished:
Reset FDC Totals
Reset Master Timer
SSR dump -> dump New
CAR #1335 2024 ISN Season & Hi Background Test Sweep Table upload
Pass#6 Upload Hi Normal Sweep Table
CAR #1383 Orbit #644 ATS Upload
IBEX_2024_099_o0644a_v001 103 commands
Results from Inertial Maneuver:
Q1 0.52846000 ActNor.EstInrToBdy[0]
Q2 0.43984300 ActNor.EstInrToBdy[1]
Q3 0.61134700 ActNor.EstInrToBdy[2]
Q4 0.39181900 ActNor.EstInrToBdy[3]
GPS sec 1395871235 ActNor.EstTime
UTC time
03/30/2024 22:00:21 output
MPS Diff
0.565 deg
MPS Cmd Vector X 0.99079000
MPS Cmd Vector Y 0.127538000
MPS Cmd Vector Z 0.045485000
CSS Angle TLM 0.831101
CSS Sun-Pointing Angle 1.662202
25 Mar 24 @16:30:00
CSS Angle TLM 0.273398
CSS Sun-Pointing Angle 0.546796
30 Mar 24 @22:00:00
Pre-Burn
Thruster 1 21696 25 Mar 24 @16:30:00
Thruster 2 21040
Thruster 3 29168
Thruster 4 29824
Post-Burn
Thruster 1 21968 30 Mar 24 @22:00:00
Thruster 2 21312
Thruster 3 29488
Thruster 4 30144
Number of Pulses
Thruster 1 272
Thruster 2 272
Thruster 3 320
Thruster 4 320
Thruster Pairs
Thruster 1 & 2 544
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
Office (703) 406-5976
IBEX MOC (703)404-7470
Cell (301) 606-1430