All,

   The perigee contacts were nominal for CMD and TLM. The inertial maneuver was successful.

The following was accomplished:

CAR # 1084 ATS upload – IBEX_2020_051_o0478a_v001 96 Cmds

SSR Dump -> Dump New

Reset Master Timer

Reset FDC Totals

Results from the Inertial maneuver:

Q1 0.64700700 ActNor.EstInrToBdy[0]

Q2 0.44940900 ActNor.EstInrToBdy[1]

Q3 0.21390700 ActNor.EstInrToBdy[2]

Q4 0.57763100 ActNor.EstInrToBdy[3]

GPS sec 1265412813 ActNor.EstTime

UTC time 02/10/2020 23:33:19 output

MPS Diff 0.562 deg

MPS Cmd Vector X 0.795094000

MPS Cmd Vector Y -0.552337000

MPS Cmd Vector Z -0.250498000

CSS Angle TLM 1.16718

CSS Sun-Pointing Angle 2.33436

  06 Feb 20 @ 17:00

CSS Angle TLM 1.378

CSS Sun-Pointing Angle 2.756

  10 Feb 20 @ 23:30

Pre-Burn

Thruster 1 3680 06 Feb 20 @ 17:00

Thruster 2 3584

Thruster 3 5072

Thruster 4 5168

Post-Burn

Thruster 1 4016 10 Feb 20 @ 23:30

Thruster 2 3872

Thruster 3 5440

Thruster 4 5584

Number of Pulses

Thruster 1 336

Thruster 2 288

Thruster 3 368

Thruster 4 416

Thruster Pairs 

Thruster 1 & 2 624

Thruster 3 & 4 784

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430