All,
The Perigee passes were nominal for CMD and TLM. The Inertial maneuver was successful.
Orbit #424 ATS was uploaded, Master reset timer was reset and Dumped the SSR
Q1 -0.10493500 ActNor.EstInrToBdy[0]
Q2 -0.72724100 ActNor.EstInrToBdy[1]
Q3 0.22009600 ActNor.EstInrToBdy[2]
Q4 0.64161400 ActNor.EstInrToBdy[3]
GPS sec 1222948429.000 ActNor.EstTime
UTC time
10/07/2018 11:53:35 output
MPS Diff
0.575
MPS Cmd Vector X -0.978852000
MPS Cmd Vector Y -0.183859000
MPS Cmd Vector Z -0.089694000
CSS Angle TLM 0.958792
CSS Sun-Pointing Angle 1.917584
4 Oct 18 @ 09:00
CSS Angle TLM 0.2074729
CSS Sun-Pointing Angle 0.4149458
7 Oct 18 @ 11:00
Pre-Burn
Thruster 1 6656 4 Oct 18 @ 09:00
Thruster 2 6496
Thruster 3 7152
Thruster 4 7312
Post-Burn
Thruster 1 6944 7 Oct 18 @ 11:00
Thruster 2 6784
Thruster 3 7456
Thruster 4 7616
Number of Pulses
Thruster 1 288
Thruster 2 288
Thruster 3 304
Thruster 4 304
Thruster Pairs
Thruster 1 & 2 576
Thruster 3 & 4 608
Timothy E. Perry
CRS, IBEX, OCO-2 & TESS
Mission Operations
Tim.perry@ngc.com
Office (703) 406-5976
Cell (301) 606-1430
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