All,

  The spacecraft is nominal. The inertial maneuver was successful. The spacecraft clock was set and the master timer was reset. The SSR was dumped. The Orbit 558 ATS was uplinked.

Tasks Accomplished:

Set Spacecraft Clock

Reset FDC Totals

Reset 18 day timer

SSR Dump -> Dump New

CAR # 1225 Orbit #558 ATS upload

   IBEX_2022_047_o0558a_v001 93 cmds

Inertial Maneuver results:

Q1 0.72579000 ActNor.EstInrToBdy[0]

Q2 0.32231100 ActNor.EstInrToBdy[1]

Q3 0.27962900 ActNor.EstInrToBdy[2]

Q4 0.53958500 ActNor.EstInrToBdy[3]

GPS sec 1328225395 ActNor.EstTime

UTC time 02/06/2022 23:29:41 output

MPS Diff 0.587 deg

MPS Cmd Vector X 0.752686000

MPS Cmd Vector Y -0.599980000

MPS Cmd Vector Z -0.271088000

CSS Angle TLM 0.819483

CSS Sun-Pointing Angle 1.638966

  03 Feb 22 @ 18:00:00

CSS Angle TLM 0.823057

CSS Sun-Pointing Angle 1.646114

  06 Feb 22 @ 23:30:00

Pre-Burn

Thruster 1 16128 03 Feb 22 @ 18:00:00

Thruster 2 15696

Thruster 3 20016

Thruster 4 20448

Post-Burn

Thruster 1 16528 06 Feb 22 @ 23:30:00

Thruster 2 16064

Thruster 3 20432

Thruster 4 20896

Number of Pulses

Thruster 1 400

Thruster 2 368

Thruster 3 416

Thruster 4 448

Thruster Pairs  

Thruster 1 & 2 768

Thruster 3 & 4 864

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430