All,
The apogee contact was nominal. The inertial maneuver was successful.
Tasks Accomplished:
Reset FDC totals
Results from the Inertial Maneuver:
Q1 0.69799500 ActNor.EstInrToBdy[0]
Q2 -0.04554130 ActNor.EstInrToBdy[1]
Q3 -0.71443000 ActNor.EstInrToBdy[2]
Q4 0.01786840 ActNor.EstInrToBdy[3]
GPS sec 1411169500 ActNor.EstTime
UTC time
09/23/2024 23:31:26 output
MPS Diff
0.844 deg
MPS Cmd Vector X -0.99918000
MPS Cmd Vector Y 0.03992200
MPS Cmd Vector Z 0.00673700
CSS Angle TLM 1.30409
CSS Sun-Pointing Angle 2.60818
18 Sept 24 @07:00:00
CSS Angle TLM 0.866601
CSS Sun-Pointing Angle 1.733202
23 Sept 24 @23:30:00
Pre-Burn
Thruster 1 6000 18 Sept 24 @07:00:00
Thruster 2 5840
Thruster 3 6784
Thruster 4 6944
Post-Burn
Thruster 1 6128 23 Sept 24 @23:30:00
Thruster 2 5968
Thruster 3 6928
Thruster 4 7088
Number of Pulses
Thruster 1 128
Thruster 2 128
Thruster 3 144
Thruster 4 144
Thruster Pairs
Thruster 1 & 2 256
Thruster 3 & 4 288
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
Office (703) 406-5976
Cell (301) 606-1430