All,

    The apogee pass was nominal for CMD and TLM. The inertial maneuver was successful.

Results from the Inertial maneuver:

Q1 0.69214000 ActNor.EstInrToBdy[0]

Q2 0.31649200 ActNor.EstInrToBdy[1]

Q3 0.44348100 ActNor.EstInrToBdy[2]

Q4 0.47339200 ActNor.EstInrToBdy[3]

MPS Cmd Vector X 0.916446000

MPS Cmd Vector Y -0.363402000

MPS Cmd Vector Z -0.167526000

GPS sec 1266775195 ActNor.EstTime

UTC time 02/26/2020 17:59:41 output

MPS Diff 0.843 deg

CSS Angle TLM 0.589171

CSS Sun-Pointing Angle 1.178342

  19 Feb 20 @ 23:30

CSS Angle TLM 0.625263

CSS Sun-Pointing Angle 1.250526

  26 Feb 20 @ 18:00

Pre-Burn

Thruster 1 4528 19 Feb 20 @ 23:30

Thruster 2 4384

Thruster 3 6096

Thruster 4 6240

Post-Burn

Thruster 1 4768 26 Feb 20 @ 18:00

Thruster 2 4624

Thruster 3 6384

Thruster 4 6528

Number of Pulses

Thruster 1 240

Thruster 2 240

Thruster 3 288

Thruster 4 288

Thruster Pairs 

Thruster 1 & 2 480

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