[Isocops] Goat Herder for 16 Dec 2019

[Perry, Timothy E [US] (IS)]

All,
    The apogee pass was nominal for CMD and TLM. The Inertial maneuver was successful. I was able to command the downlink to 40k. The star tracker had reset in the back orbit. I executed Standing CAR #344 Reset FDC Totals and Response Latch Values. The star tracker had recovered nominally and the STA Percent valid was at 80.


Results from the Inertial maneuver:
Q1 0.41501300 ActNor.EstInrToBdy[0]
Q2 -0.72453500 ActNor.EstInrToBdy[1]
Q3 0.42438900 ActNor.EstInrToBdy[2]
Q4 0.35029500 ActNor.EstInrToBdy[3]
GPS sec 1260495170 ActNor.EstTime
UTC time 12/16/2019 01:32:36 output
MPS Diff 0.451 deg
MPS Cmd Vector X -0.153733000
MPS Cmd Vector Y -0.902885000
MPS Cmd Vector Z -0.401452000
CSS Angle TLM 0.513581
CSS Sun-Pointing Angle 1.027162
  07 Dec 19 @ 05:00
CSS Angle TLM 0.289391
CSS Sun-Pointing Angle 0.578782
  16 Dec 19 @ 01:30
Pre-Burn
Thruster 1 416 07 Dec 19 @ 05:00
Thruster 2 416
Thruster 3 432
Thruster 4 432
Post-Burn
Thruster 1 704 16 Dec 19 @ 01:30
Thruster 2 704
Thruster 3 752
Thruster 4 752
Number of Pulses
Thruster 1 288
Thruster 2 288
Thruster 3 320
Thruster 4 320
Thruster Pairs
Thruster 1 & 2 576
Thruster 3 & 4 640



Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
timothy.perry at ngc.com
Office (703) 406-5976
Cell (301) 606-1430

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