All,
The perigee Contacts were nominal. The inertial maneuver was successful. Both Orbit’s 671 & 672 ATS’s have been uploaded. The SSR was dumped, and all the
missing data was redumped.
Tasks Accomplished:
Reset FDC Totals
Set Spacecraft Clock
Dumped Orbit 670 Data
Reset Master Timer
CAR# 1434 Orbit 671 ATS Upload
CAR# 1436 Orbit 672 ATS upload
CAR# 1435 Hi Sweep Contact ATS upload
CAR# 1432 Redump Orbit 669 Blocks
CAR# 1437 Redump Orbit 670 Blocks
Results from the Inertial Maneuver:
Q1 0.63343700 ActNor.EstInrToBdy[0]
Q2 -0.54160000 ActNor.EstInrToBdy[1]
Q3 0.26913700 ActNor.EstInrToBdy[2]
Q4 0.48269300 ActNor.EstInrToBdy[3]
GPS sec 1417854619 ActNor.EstTime
UTC time
12/10/2024 08:30:05 output
MPS Diff
0.756 deg
MPS Cmd Vector X -0.17639300
MPS Cmd Vector Y -0.89916800
MPS Cmd Vector Z -0.40047700
CSS Angle TLM 1.31656
CSS Sun-Pointing Angle 2.63312
06 Dec 24 @19:00:00
CSS Angle TLM 0.85257
CSS Sun-Pointing Angle 1.70514
10 Dec 24 @08:30:00
Pre-Burn
Thruster 1 10288 06 Dec 24 @19:00:00
Thruster 2 10032
Thruster 3 12736
Thruster 4 12992
Post-Burn
Thruster 1 10688 10 Dec 24 @08:30:00
Thruster 2 10384
Thruster 3 13104
Thruster 4 13408
Number of Pulses
Thruster 1 400
Thruster 2 352
Thruster 3 368
Thruster 4 416
Thruster Pairs
Thruster 1 & 2 752
Thruster 3 & 4 784
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
Office (703) 406-5976
IBEX MOC (703)404-7470
Cell (301) 606-1430