All,
The perigee contacts were nominal for CMD and TLM. The Inertial maneuver was successful.
The following was completed:
SSR Dump
Flight Computer Back Orbit Dump
Reset Master Timer
CAR # 1005 ATS upload
IBEX_2018_325_o0426a_V001
91 Cmds Trk # 503-593
Q1 0.59224800 ActNor.EstInrToBdy[0]
Q2 0.54123500 ActNor.EstInrToBdy[1]
Q3 -0.59659700 ActNor.EstInrToBdy[2]
Q4 0.01946490 ActNor.EstInrToBdy[3]
GPS sec 1226061220.000 ActNor.EstTime
MPS Cmd Vector X -0.681259000
MPS Cmd Vector Y -0.667931000
MPS Cmd Vector Z -0.299590000
MPS Diff
0.744 deg
CSS Angle TLM
0.604579
CSS Sun-Pointing Angle
1.209158
08 Nov 18 @ 23:00
CSS Angle TLM
0.696612
CSS Sun-Pointing Angle
1.393224
12 Nov 18 @ 12:30
Number of Pulses
12 Nov 18 @ 12:30
Thruster 1
272
Thruster 2
272
Thruster 3
288
Thruster 4
288
Thruster Pairs
Thruster 1 & 2
544
Thruster 3 & 4
576
Timothy E. Perry
Mission Operations
CRS, IBEX, OCO-2 & TESS
RAPTOR Test Team
timothy.perry@ngc.com
Office (703) 406-5976
Cell (301) 606-1430
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