All,

      The apogee contact was nominal for CMD & TLM. The inertial maneuver was successful. The orbit 508 Bus and Inst ATS’s have been uplinked. Current timed cmd counter is @224.

Task’s accomplished:

CAR # 1130 ATS upload

IBEX_20202_323_o0508a_BUS_V001 46 CMDS

IBEX_20202_323_o0508a_INST_V001 46 CMDS

Inertial Maneuver Results:

Q1 -0.16178500 ActNor.EstInrToBdy[0]

Q2 -0.77696700 ActNor.EstInrToBdy[1]

Q3 0.46519100 ActNor.EstInrToBdy[2]

Q4 0.39210400 ActNor.EstInrToBdy[3]

GPS sec 1288744305 ActNor.EstTime

UTC time 11/07/2020 00:31:31 output

MPS Cmd Vector X -0.760177000

MPS Cmd Vector Y -0.592037000

MPS Cmd Vector Z -0.267625000

MPS Diff 0.508 deg

CSS Angle TLM 0.701929

CSS Sun-Pointing Angle 1.403858

01 Nov 20 @ 00:05:00

CSS Angle TLM 1.15148

CSS Sun-Pointing Angle 2.30296

07 Nov 20 @ 00:30:00

Pre-Burn

Thruster 1 6768 01 Nov 20 @ 00:05:00

Thruster 2 6592

Thruster 3 8240

Thruster 4 8416

Post-Burn `

Thruster 1 6912 07 Nov 20 @ 00:30:00

Thruster 2 6736

Thruster 3 8432

Thruster 4 8608

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