All
The Apogee pass was nominal for CMD and TLM and the inertial maneuver was successful.
Q1 -0.28620700 ActNor.EstInrToBdy[0]
Q2 -0.47179600 ActNor.EstInrToBdy[1]
Q3 -0.63096800 ActNor.EstInrToBdy[2]
Q4 0.54532000 ActNor.EstInrToBdy[3]
GPS sec
1214657977.000 ActNor.EstTime
MPS Diff
0.661
MPS Cmd Vector X -0.161561000
MPS Cmd Vector Y 0.909481000
MPS Cmd Vector Z 0.383070000
CSS Angle TLM 4.75992
CSS Sun-Pointing Angle 9.51984
29 June18 @1830
CSS Angle TLM 0.345484
CSS Sun-Pointing Angle 0.690968
3 July @ 1300
Pre-Burn
Thruster 1 864 29 June18 @1830
Thruster 2 832
Thruster 3 880
Thruster 4 912
Post-Burn
Thruster 1 1136 3 July @ 1300
Thruster 2 1104
Thruster 3 1168
Thruster 4 1200
Number of Pulses
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
CRS, IBEX, OCO-2 & TESS
Mission Operations
Tim.perry@ngc.com
Office (703) 406-5976
Cell (301) 606-1430
Corp Cell (571) 447-8977
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