All,

    The spacecraft is nominal. The inertial maneuver was successful.

Results from the Inertial maneuver:

Q1 0.53161600 ActNor.EstInrToBdy[0]

Q2 -0.40404700 ActNor.EstInrToBdy[1]

Q3 -0.68624700 ActNor.EstInrToBdy[2]

Q4 0.28843700 ActNor.EstInrToBdy[3]

GPS sec 1315274834 ActNor.EstTime

UTC time 09/10/2021 02:07:00 output

MPS Diff 0.746 deg

MPS Cmd Vector X -0.964643000

MPS Cmd Vector Y 0.245616000

MPS Cmd Vector Z 0.095585000

CSS Angle TLM 1.537

CSS Sun-Pointing Angle 3.074

  05 Sept 21 @ 19:\30:00

CSS Angle TLM 0.330431

CSS Sun-Pointing Angle 0.660862

  10 Sept 21 @ 02:00:00

Pre-Burn

Thruster 1 7808 05 Sept 21 @ 19:\30:00

Thruster 2 7648

Thruster 3 8672

Thruster 4 8832

Post-Burn

Thruster 1 8096 10 Sept 21 @ 02:00:00

Thruster 2 7904

Thruster 3 8960

Thruster 4 9152

Number of Pulses

Thruster 1 288

Thruster 2 256

Thruster 3 288

Thruster 4 320

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