All,
The Apogee pass was nominal for CMD and TLM. The Inertial maneuver was successful.
Q1 -0.48524900
ActNor.EstInrToBdy[0]
Q2 -0.26136200
ActNor.EstInrToBdy[1]
Q3 -0.28474200
ActNor.EstInrToBdy[2]
Q4 0.78431200
ActNor.EstInrToBdy[3]
GPS sec 1246107709
ActNor.EstTime
UTC time
07/02/2019 13:01:35 output
MPS Cmd Vector X -0.141023000
MPS Cmd Vector Y 0.912322000
MPS Cmd Vector Z 0.384424000
MPS Diff
0.637 deg
CSS Angle TLM 1.26594
CSS Sun-Pointing Angle 2.53188
28 June 19 @ 03:00
CSS Angle TLM 0.173589
CSS Sun-Pointing Angle 0.347178
02 July 19 @ 13:00
Pre-Burn
Thruster 1 13696 28 June 19 @ 03:00
Thruster 2 13376
Thruster 3 16224
Thruster 4 16544
Post-Burn
Thruster 1 13952 02 July 19 @ 13:00
Thruster 2 13632
Thruster 3 16496
Thruster 4 16816
Number of Pulses
Thruster 1 256
Thruster 2 256
Thruster 3 272
Thruster 4 272
Thruster Pairs
Thruster 1 & 2 512
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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