All,
The perigee contacts were nominal. The inertial maneuver was successful. We were able to achieve 320k downlink, so we were able to dump all the SSR data for orbits 619 & 620. The Lo sweep table was changed from magnetotail sweep
to normal sweep. The ATS for orbit 622 was uplinked.
Tasks Accomplished:
Reset FDC Totals
Reset the Master Timer
SSR Dump -> Dump New
CAR #1301 IBEX Background test and Lo 2023 Magnetotail season
Pass #3 Upload Lo Normal Sweep Table
CAR #1339 Orbit 622 ATS upload
IBEX_2023_264_o0622a_v001 91 commands
Results from the Inertial Maneuver:
Q1 0.14480300 ActNor.EstInrToBdy[0]
Q2 -0.65580700 ActNor.EstInrToBdy[1]
Q3 -0.31847900 ActNor.EstInrToBdy[2]
Q4 0.66897000 ActNor.EstInrToBdy[3]
GPS sec 1378569657 ActNor.EstTime
UTC time
09/12/2023 16:00:43 output
MPS Diff
0.773 deg
MPS Cmd Vector X -0.97186800
MPS Cmd Vector Y 0.219519000
MPS Cmd Vector Z 0.085347000
CSS Angle TLM 0.224684
CSS Sun-Pointing Angle 0.449368
07 Sept 23@07:00:00
CSS Angle TLM 0.484164
CSS Sun-Pointing Angle 0.968328
12 Sept 23@16:00:00
Pre-Burn
Thruster 1 11280 07 Sept 23@07:00:00
Thruster 2 11008
Thruster 3 13488
Thruster 4 13760
Post-Burn
Thruster 1 11552 12 Sept 23@16:00:00
Thruster 2 11280
Thruster 3 13792
Thruster 4 14064
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
Cell (301) 606-1430