All,

   The apogee contact was nominal for CMD & TLM. The inertial maneuver was successful.

Results from the Inertial Maneuver:

Q1 -0.24295100 ActNor.EstInrToBdy[0]

Q2 0.49643300 ActNor.EstInrToBdy[1]

Q3 0.81741400 ActNor.EstInrToBdy[2]

Q4 0.16236900 ActNor.EstInrToBdy[3]

GPS sec 1309781213 ActNor.EstTime

UTC time 07/08/2021 12:06:39 output

MPS Diff 0.871 deg

MPS Cmd Vector X -0.243985000

MPS Cmd Vector Y 0.893698000

MPS Cmd Vector Z 0.376531000

CSS Angle TLM 1.1955

CSS Sun-Pointing Angle 2.391

  03 July 21 @ 21:00:00

CSS Angle TLM 0.370094

CSS Sun-Pointing Angle 0.740188

  08 July 21 @ 12:00:00

Pre-Burn

Thruster 1 4096 03 July 21 @ 21:00:00

Thruster 2 4000

Thruster 3 4528

Thruster 4 4624

Post-Burn

Thruster 1 4352 08 July 21 @ 12:00:00

Thruster 2 4256

Thruster 3 4816

Thruster 4 4912

Number of Pulses

Thruster 1 256

Thruster 2 256

Thruster 3 288

Thruster 4 288

Thruster Pairs 

Thruster 1 & 2 512

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