All,

    The apogee contact was nominal for CMD and TLM. The Inertial maneuver was successful.. The Orbit 503 Version 2 Bus ATS was uplinked.

Tasks accomplished:

CAR # 1120 ATS Upload.

    IBEX_2020_278_o0503a_BUS_V002 55 Cmds

Results from the Inertial Maneuver:

Q1 0.68264100 ActNor.EstInrToBdy[0]

Q2 -0.12354800 ActNor.EstInrToBdy[1]

Q3 -0.71649600 ActNor.EstInrToBdy[2]

Q4 0.07327930 ActNor.EstInrToBdy[3]

GPS sec 1284606165 ActNor.EstTime

UTC time 09/20/2020 03:02:31 output

MPS Diff 0.812 deg

MPS Cmd Vector X -0.996566000

MPS Cmd Vector Y 0.079394000

MPS Cmd Vector Z 0.023507000

CSS Angle TLM 0.679262

CSS Sun-Pointing Angle 1.358524

  16 Sept 20 @ 06:30:00

CSS Angle TLM 0.144018

CSS Sun-Pointing Angle 0.288036

  20 Sept 20 @ 03:00:00

Pre-Burn

Thruster 1 4176 16 Sept 20 @ 06:30:00

Thruster 2 4048

Thruster 3 4768

Thruster 4 4896

Post-Burn   `

Thruster 1 4448 20 Sept 20 @ 03:00:00

Thruster 2 4320

Thruster 3 5072

Thruster 4 5200

Number of Pulses

Thruster 1 272

Thruster 2 272

Thruster 3 304

Thruster 4 304

Thruster Pairs 

Thruster 1 & 2 544

Thruster 3 & 4 608

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430