All,

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

The following tasks were accomplished:

SSR Dump -> Dump New

Reset Master Timer

Set Spacecraft Clock

Reset FDC totals

CAR # 1081 ATS Upload – IBEX_2020_023_o0475a_v001 96 cmds

Results from the Inertial Maneuver:

Q1 -0.10874100 ActNor.EstInrToBdy[0]

Q2 0.81775300 ActNor.EstInrToBdy[1]

Q3 -0.53516900 ActNor.EstInrToBdy[2]

Q4 0.18179800 ActNor.EstInrToBdy[3]

GPS sec 1263006327 ActNor.EstTime

UTC time 01/14/2020 03:05:13 output

MPS Cmd Vector X 0.414375000

MPS Cmd Vector Y -0.830927000

MPS Cmd Vector Z -0.371287000

MPS Diff 0.646 deg

CSS Angle TLM 1.16634

CSS Sun-Pointing Angle 2.33268

  9 Jan 20 @ 18:00

CSS Angle TLM 1.72762

CSS Sun-Pointing Angle 3.45524

  13 Jan 20 @ 3:00

Pre-Burn

Thruster 1 2048 9 Jan 20 @ 18:00

Thruster 2 2000

Thruster 3 2992

Thruster 4 3040

Post-Burn

Thruster 1 2448 13 Jan 20 @ 3:00

Thruster 2 2352

Thruster 3 3360

Thruster 4 3456

Number of Pulses

Thruster 1 400

Thruster 2 352

Thruster 3 368

Thruster 4 416

Thruster Pairs 

Thruster 1 & 2 752

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