All,
The perigee contacts were nominal. We had a few errors on the SSR dump, we were able to redump the missing data on the second contact. The missing data
for orbit 664 was also redumped with zero errors. The Orbit 667 ATS was uplinked, and the inertial maneuver was successful. The star tracker reset time was 17 Oct 24 @00:12:12gmt.
Tasks Accomplished:
SSR Dump -> Dump New
Reset FDC Totals
Reset Master Timer
CAR #1421 Redump Orbit 664 SSR Blocks
CAR #1422 Orbit #667 ATS upload
IBEX_2024_308_o0667a_v001 98 Cmd
CAR #1423 Redump Orbit 665 SSR Blocks
Results from the Inertial Maneuver:
Q1 0.76551100 ActNor.EstInrToBdy[0]
Q2 0.10782700 ActNor.EstInrToBdy[1]
Q3 -0.59730700 ActNor.EstInrToBdy[2]
Q4 0.21352000 ActNor.EstInrToBdy[3]
GPS sec 1413873253 ActNor.EstTime
UTC time
10/25/2024 06:33:59 output
MPS Diff
0.656 deg
MPS Cmd Vector X -0.86690300
MPS Cmd Vector Y -0.45372600
MPS Cmd Vector Z -0.20642600
CSS Angle TLM 0.510141
CSS Sun-Pointing Angle 1.020282
20 Oct 24 @20:00:00
CSS Angle TLM 0.817571
CSS Sun-Pointing Angle 1.635142
25 Oct 24 @02:30:00
Pre-Burn
Thruster 1 7584 20 Oct 24 @20:00:00
Thruster 2 7376
Thruster 3 9104
Thruster 4 9312
Post-Burn
Thruster 1 7856 25 Oct 24 @02:30:00
Thruster 2 7648
Thruster 3 9408
Thruster 4 9616
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