All,

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

Results from the Inertial Maneuver:

Q1 -0.59527600 ActNor.EstInrToBdy[0]

Q2 0.19120900 ActNor.EstInrToBdy[1]

Q3 0.76118500 ActNor.EstInrToBdy[2]

Q4 0.17228700 ActNor.EstInrToBdy[3]

GPS sec 1313721191 ActNor.EstTime

UTC time 08/23/2021 02:32:57 output

MPS Cmd Vector X -0.842062000

MPS Cmd Vector Y 0.498768000

MPS Cmd Vector Z 0.205333000

MPS Diff 0.757 deg

CSS Angle TLM 0.290066

CSS Sun-Pointing Angle 0.580132

18 Aug 21 @ 18:00:00

CSS Angle TLM 0.408304

CSS Sun-Pointing Angle 0.816608

23 Aug 21 @ 02:30:00

Pre-Burn

Thruster 1 6752 14 Aug 21 @ 03:00:00

Thruster 2 6352

Thruster 3 7200

Thruster 4 7328

Post-Burn

Thruster 1 6992 23 Aug 21 @ 02:30:00

Thruster 2 6832

Thruster 3 7808

Thruster 4 7968

Number of Pulses

Thruster 1 240

Thruster 2 480

Thruster 3 608

Thruster 4 640

Thruster Pairs

Thruster 1 & 2 720

Thruster 3 & 4 1248

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430