All,

    The apogee contact was nominal for CMD and TLM. The Inertial maneuver was successful.

The following was accomplished:

CAR 1095 ATS upload – IBEX_2020_133_o0487a_INST_V001 46 cmds

Results from the Inertial Maneuver:

Q1 -0.57264600 ActNor.EstInrToBdy[0]

Q2 -0.18765800 ActNor.EstInrToBdy[1]

Q3 -0.73539900 ActNor.EstInrToBdy[2]

Q4 0.30992000 ActNor.EstInrToBdy[3]

GPS sec 1272806651 ActNor.EstTime

UTC time 05/06/2020 13:23:57 output

MPS Cmd Vector X 0.723236000

MPS Cmd Vector Y 0.637573000

MPS Cmd Vector Z 0.265388000

MPS Diff 0.628 deg

CSS Angle TLM 0.664996

CSS Sun-Pointing Angle 1.329992

  02 May 20 @ 04:30

CSS Angle TLM 0.359365

CSS Sun-Pointing Angle 0.71873

  06 May 20 @ 03:00

Pre-Burn

Thruster 1 8544 02 May 20 @ 04:30

Thruster 2 8272

Thruster 3 11056

Thruster 4 11328

Post-Burn

Thruster 1 8672 06 May 20 @ 03:00

Thruster 2 8400

Thruster 3 11216

Thruster 4 11488

Number of Pulses

Thruster 1 128

Thruster 2 128

Thruster 3 160

Thruster 4 160

Thruster Pairs 

Thruster 1 & 2 256

Thruster 3 & 4 320

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430