All,

    The apogee contact was nominal for CMD & TLM. The inertial maneuver was successful. The Orbit #504 Battery Balancing ATS and Hi High Gain Cal ATS was uplinked.

Tasks Accomplished:

CAR # 1123 ATS Upload

   IBEX_2020_287_o0504a_HGC_V001 64 Cmds

CAR # 1124 ATS Upload

   IBEX_2020_287_o0504a_Bat_Bal_V001 2 Cmds

Results from the Inertial maneuver:

Q1 0.65931100 ActNor.EstInrToBdy[0]

Q2 -0.33438500 ActNor.EstInrToBdy[1]

Q3 -0.52140800 ActNor.EstInrToBdy[2]

Q4 0.42618100 ActNor.EstInrToBdy[3]

GPS sec 1286236344 ActNor.EstTime

UTC time 10/08/2020 23:52:10 output

MPS Cmd Vector X -0.973015000

MPS Cmd Vector Y -0.207513000

MPS Cmd Vector Z -0.100900000

MPS Diff 0.558 deg

CSS Angle TLM 1.63327

CSS Sun-Pointing Angle 3.26654

04 Oct 20 @ 08:00:00

CSS Angle TLM 0.0791294

CSS Sun-Pointing Angle 0.1582588

08 Oct 20 @ 23:30:00

Pre-Burn

Thruster 1 5264 04 Oct 20 @ 08:00:00

Thruster 2 5136

Thruster 3 6240

Thruster 4 6368

Post-Burn `

Thruster 1 5408 08 Oct 20 @ 23:30:00

Thruster 2 5280

Thruster 3 6432

Thruster 4 6560

Number of Pulses

Thruster 1 144

Thruster 2 144

Thruster 3 192

Thruster 4 192

Thruster Pairs

Thruster 1 & 2 288

Thruster 3 & 4 384

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430