All,

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

Results from the Inertial Maneuver:

Q1 -0.40660500 ActNor.EstInrToBdy[0]

Q2 -0.40598700 ActNor.EstInrToBdy[1]

Q3 -0.16557600 ActNor.EstInrToBdy[2]

Q4 0.80151800 ActNor.EstInrToBdy[3]

GPS sec 1311394618 ActNor.EstTime

UTC time 07/27/2021 04:16:44 output

MPS Diff 0.631 deg

MPS Cmd Vector X -0.521706000

MPS Cmd Vector Y 0.786660000

MPS Cmd Vector Z 0.330136000

CSS Angle TLM 0.488189

CSS Sun-Pointing Angle 0.976378

  22 Jul 21 @ 12:30:00

CSS Angle TLM 1.80515

CSS Sun-Pointing Angle 3.6103

  27 Jul 21 @ 04:00:00

Pre-Burn

Thruster 1 5152 22 Jul 21 @ 12:30:00

Thruster 2 5024

Thruster 3 5728

Thruster 4 5856

Post-Burn

Thruster 1 5424 27 Jul 21 @ 04:00:00

Thruster 2 5296

Thruster 3 6000

Thruster 4 6128

Number of Pulses

Thruster 1 272

Thruster 2 272

Thruster 3 272

Thruster 4 272

Thruster Pairs  

Thruster 1 & 2 544

Thruster 3 & 4 544

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430