All,

    The apogee contact was nominal for CMD and TLM. The inertial maneuver was successful. The Orbit #500 Bus ATS was uplinked.

Tasks accomplished:

CAR #1112 ATS Upload

   IBEX_2020_250_o0500a_BUS_V001 53 commands

Results from the Inertial maneuver:

Q1 -0.02082860 ActNor.EstInrToBdy[0]

Q2 -0.62799400 ActNor.EstInrToBdy[1]

Q3 -0.36479900 ActNor.EstInrToBdy[2]

Q4 0.68710400 ActNor.EstInrToBdy[3]

GPS sec 1282212148 ActNor.EstTime

UTC time 08/23/2020 10:02:14 output

MPS Diff 0.623 deg

MPS Cmd Vector X -0.850679000

MPS Cmd Vector Y 0.486203000

MPS Cmd Vector Z 0.199881000

CSS Angle TLM 0.300666

CSS Sun-Pointing Angle 0.601332

  19 Aug 20 @ 04:00

CSS Angle TLM 1.29

CSS Sun-Pointing Angle 2.58

  23 Aug 20 @ 10:00

Pre-Burn

Thruster 1 2560 19 Aug 20 @ 04:00

Thruster 2 2464

Thruster 3 2912

Thruster 4 3008

Post-Burn   `

Thruster 1 2832 23 Aug 20 @ 10:00

Thruster 2 2736

Thruster 3 3200

Thruster 4 3296

Number of Pulses

Thruster 1 272

Thruster 2 272

Thruster 3 288

Thruster 4 288

Thruster Pairs 

Thruster 1 & 2 544

Thruster 3 & 4 576

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430