All,
The Apogee pass was nominal for Cmd and tlm. The Inertial maneuver was successful.
Q1 -0.15642300 ActNor.EstInrToBdy[0]
Q2 0.53356400 ActNor.EstInrToBdy[1]
Q3 0.67676800 ActNor.EstInrToBdy[2]
Q4 0.48252000 ActNor.EstInrToBdy[3]
GPS sec
1212327480.000 ActNor.EstTime
MPS Cmd Vector X 0.296911000
MPS Cmd Vector Y 0.880170000
MPS Cmd Vector Z 0.370330000
MPS Diff
0.846
01 June18 @01300
CSS Angle TLM 0.538867
CSS Sun-Pointing Angle 1.077734
06 June18 @01300
CSS Angle TLM 0.733287
CSS Sun-Pointing Angle 1.466574
Pre-Burn
01 June18 @01300
Thruster 1 1936
Thruster 2 1904
Thruster 3 2080
Thruster 4 2112
Post-Burn
06 June18 @01300
Thruster 1 2240
Thruster 2 2176
Thruster 3 2368
Thruster 4 2432
Number of Pulses
Thruster 1 304
Thruster 2 272
Thruster 3 288
Thruster 4 320
Thruster Pairs
Thruster 1 & 2 576
Thruster 3 & 4 608
Timothy E. Perry
CRS, IBEX, OCO-2 & TESS
Mission Operations
Tim.perry@orbitalatk.com
Office (703) 406-5976
Cell (301) 606-1430
Corp Cell (571) 447-8977
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