All,
The Apogee pass was nominal for CMD and TLM. The Inertial maneuver was nominal.
Results from the maneuver:
Q1 -0.49558900
ActNor.EstInrToBdy[0]
Q2 -0.25282600
ActNor.EstInrToBdy[1]
Q3 -0.13334300
ActNor.EstInrToBdy[2]
Q4 0.82017700
ActNor.EstInrToBdy[3]
GPS sec 1246885532
ActNor.EstTime
UTC time 07/11/2019 13:05:18 output
MPS Diff 0.635
deg
MPS Cmd Vector X -0.287926000
MPS Cmd Vector Y 0.882632000
MPS Cmd Vector Z 0.371562000
CSS Angle TLM 1.47631
CSS Sun-Pointing Angle 2.95262
07 July 19 @ 06:30
CSS Angle TLM 1.57483
CSS Sun-Pointing Angle 3.14966
11 July 19 @ 13:00
Pre-Burn
Thruster 1 14288 07 July 19 @ 06:30
Thruster 2 13904
Thruster 3 16800
Thruster 4 17184
Post-Burn
Thruster 1 14544 11 July 19 @ 13:00
Thruster 2 14160
Thruster 3 17072
Thruster 4 17456
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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