All,
The apogee pass was nominal for CMD and TLM. The Inertial maneuver was successful. The Orbit #494 Instrument ATS was uplinked.
Tasks Accomplished:
CAR #2003 ATS Upload -> IBEX_2020_194_o0494a_INST_V001 46 CMDS
Inertial Maneuver Results:
Q1 -0.41314800
ActNor.EstInrToBdy[0]
Q2 -0.36485900
ActNor.EstInrToBdy[1]
Q3 -0.48792000
ActNor.EstInrToBdy[2]
Q4 0.67684600
ActNor.EstInrToBdy[3]
GPS sec 1277467300
ActNor.EstTime
UTC time 06/29/2020 12:01:26 output
MPS Diff 0.367
deg
MPS
Cmd Vector X -0.092726000
MPS
Cmd Vector Y 0.917493000
MPS
Cmd Vector Z 0.386791000
CSS Angle TLM 2.49
CSS Sun-Pointing Angle 4.98
24 June 20 @ 15:00
CSS Angle TLM 1.63996
CSS Sun-Pointing Angle 3.27992
29 June 20 @ 12:00
Pre-Burn
Thruster 1 11600 24 June 20 @ 15:00
Thruster 2 11296
Thruster 3 14386
Thruster 4 14672
Post-Burn
Thruster 1 11904 29 June 20 @ 12:00
Thruster 2 11568
Thruster 3 14672
Thruster 4 15008
Number of Pulses
Thruster 1 304
Thruster 2 272
Thruster 3 286
Thruster 4 336
Thruster Pairs
Thruster 1 & 2 576
Thruster 3 & 4 622
Timothy E. Perry
Mission Operations
CRS, IBEX, OCO-2
Office (703) 406-5976
Cell (301) 606-1430
