All,

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

The following was accomplished:

CAR # 1063 – ISN Season & Hi Background sweep table uploads

   Completed Pass 5 – Upload Normal Sweep table

CAR # 1082 – ATS Upload – IBEX_2020_032_o0476a_v001 88 Cmds

SSR Dump -> Dump New

Flight Computer Back orbit Dump

Reset Master Timer

Set Spacecraft Time

Reset FDC Totals

Results from the Inertial maneuver:

Q1 0.74043800 ActNor.EstInrToBdy[0]

Q2 -0.34084600 ActNor.EstInrToBdy[1]

Q3 0.50497000 ActNor.EstInrToBdy[2]

Q4 0.28386900 ActNor.EstInrToBdy[3]

GPS sec 1263841326 ActNor.EstTime

UTC time 01/23/2020 19:01:52 output

MPS Cmd Vector X 0.556953000

MPS Cmd Vector Y -0.757923000

MPS Cmd Vector Z -0.339641000

MPS Diff 0.743 deg

CSS Angle TLM 1.05388

CSS Sun-Pointing Angle 2.10776

  19 Jan 20 @ 1:00

CSS Angle TLM 0.716005

CSS Sun-Pointing Angle 1.43201

  23 Jan 20 @ 19:00

Pre-Burn

Thruster 1 2544 19 Jan 20 @ 1:00

Thruster 2 2448

Thruster 3 3780

Thruster 4 3856

Post-Burn

Thruster 1 2864 23 Jan 20 @ 19:00

Thruster 2 2768

Thruster 3 4128

Thruster 4 4224

Number of Pulses

Thruster 1 320

Thruster 2 320

Thruster 3 348

Thruster 4 368

Thruster Pairs 

Thruster 1 & 2 640

Thruster 3 & 4 716

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430