All,
The apogee contact was nominal for command and telemetry. The inertial maneuver was successful.
Tasks Accomplished:
Reser FDC Totals
Results from the Inertial Maneuver:
Q1 0.13669300 ActNor.EstInrToBdy[0]
Q2 0.56182100 ActNor.EstInrToBdy[1]
Q3 0.75216300 ActNor.EstInrToBdy[2]
Q4 0.31610600 ActNor.EstInrToBdy[3]
GPS sec 1400158863 ActNor.EstTime
UTC time
05/19/2024 13:00:49 output
MPS Diff
0.815 deg
MPS Cmd Vector X 0.55439900
MPS Cmd Vector Y 0.76742200
MPS Cmd Vector Z 0.32203400
CSS Angle TLM 0.3743
CSS Sun-Pointing Angle 0.7486
14 May 24 @22:00:00
CSS Angle TLM 0.0625573
CSS Sun-Pointing Angle 0.1251146
14 May 24 @22:00:00
Pre-Burn
Thruster 1 24736 14 May 24 @22:00:00
Thruster 2 24016
Thruster 3 32480
Thruster 4 33200
Post-Burn
Thruster 1 24992 19 May 24 @13:00:00
Thruster 2 24272
Thruster 3 32736
Thruster 4 33456
Number of Pulses
Thruster 1 256
Thruster 2 256
Thruster 3 256
Thruster 4 256
Thruster Pairs
Thruster 1 & 2 512
Thruster 3 & 4 512
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
Office (703) 406-5976
IBEX MOC (703)404-7470
Cell (301) 606-1430