All,
The apogee pass was nominal for CMD and TLM. The inertial maneuver was successful.
Q1 -0.53625900
ActNor.EstInrToBdy[0]
Q2 0.11549100
ActNor.EstInrToBdy[1]
Q3 0.16416000
ActNor.EstInrToBdy[2]
Q4 0.81984100
ActNor.EstInrToBdy[3]
GPS sec
1245416767.000 ActNor.EstTime
MPS Diff
0.651 deg
MPS Cmd Vector X 0.009441000
MPS Cmd Vector Y 0.921463000
MPS Cmd Vector Z 0.388352000
CSS Angle TLM 0.659382
CSS Sun-Pointing Angle 1.318764
19 June 19 @ 19:00
CSS Angle TLM 0.737544
CSS Sun-Pointing Angle 1.475088
24 June 19 @ 13:00
Pre-Burn
Thruster 1 13152 19 June 19 @ 19:00
Thruster 2 12832
Thruster 3 15648
Thruster 4 15968
Post-Burn
Thruster 1 13424 24 June 19 @ 13:00
Thruster 2 13104
Thruster 3 15920
Thruster 4 16240
Number of Pulses
Thruster 1 272
Thruster 2 272
Thruster 3 272
Thruster 4 272
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 544
Timothy E. Perry
Mission Operations
CRS, IBEX, OCO-2 & TESS
timothy.perry@ngc.com
Office (703) 406-5976
Cell (301) 606-1430
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