All,
The apogee contact was nominal. The inertial maneuver was successful. The orbit 641 ATS was uplinked.
Tasks Accomplished:
CAR #1380 Orbit #641 ATS uplink
IBEX_2024_072_o0641a_v001 103 Commands
Reset FDC Totals
Results from the Inertial Maneuver:
Q1 -0.50877000 ActNor.EstInrToBdy[0]
Q2 0.53187900 ActNor.EstInrToBdy[1]
Q3 -0.55042800 ActNor.EstInrToBdy[2]
Q4 0.39406400 ActNor.EstInrToBdy[3]
GPS sec 1393866094 ActNor.EstTime
UTC time
03/07/2024 17:01:20 output
MPS Diff
0.352 deg
MPS Cmd Vector X 0.97952300
MPS Cmd Vector Y -0.180907000
MPS Cmd Vector Z -0.088355000
CSS Angle TLM 0.86818
CSS Sun-Pointing Angle 1.73636
03 Mar 24 @06:00:00
CSS Angle TLM 1.12106
CSS Sun-Pointing Angle 2.24212
07 Mar 24 @17:00:00
Pre-Burn
Thruster 1 20512 03 Mar 24 @06:00:00
Thruster 2 19856
Thruster 3 27856
Thruster 4 28512
Post-Burn
Thruster 1 20784 07 Mar 24 @17:00:00
Thruster 2 20128
Thruster 3 28160
Thruster 4 28816
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