All,

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

Results from the Inertial Maneuver:

Q1 -0.60409000 ActNor.EstInrToBdy[0]

Q2 -0.05891970 ActNor.EstInrToBdy[1]

Q3 0.56811900 ActNor.EstInrToBdy[2]

Q4 0.55573700 ActNor.EstInrToBdy[3]

GPS sec 1312945572 ActNor.EstTime

UTC time 08/14/2021 03:05:58 output

MPS Diff 0.636 deg

MPS Cmd Vector X -0.752283000

MPS Cmd Vector Y 0.608383000

MPS Cmd Vector Z 0.252863000

CSS Angle TLM 1.222

CSS Sun-Pointing Angle 2.444

  09 Aug 21 @ 19:00:00

CSS Angle TLM 0.301965

CSS Sun-Pointing Angle 0.60393

  14 Aug 21 @ 03:00:00

Pre-Burn

Thruster 1 6240 09 Aug 21 @ 19:00:00

Thruster 2 6112

Thruster 3 6912

Thruster 4 7040

Post-Burn

Thruster 1 6480 14 Aug 21 @ 03:00:00

Thruster 2 6352

Thruster 3 7200

Thruster 4 7328

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