All,

    The perigee passes were nominal for CMD and TLM. The Inertial maneuver was successful. The SSR and Flight Computer Back Orbit Buffer was dumped. The 18 Day Master Timer reset command executed and the count back to 10.

Results from the Inertial Maneuver:

Q1 0.01592180 ActNor.EstInrToBdy[0]

Q2 -0.55725000 ActNor.EstInrToBdy[1]

Q3 -0.78861700 ActNor.EstInrToBdy[2]

Q4 0.25942600 ActNor.EstInrToBdy[3]

GPS sec 1278602641 ActNor.EstTime

MPS Cmd Vector X -0.316162000

MPS Cmd Vector Y 0.873961000

MPS Cmd Vector Z 0.369098000

MPS Diff 0.579 deg

CSS Angle TLM 1.50024

CSS Sun-Pointing Angle 3.00048

9 July 20 @ 12:00

CSS Angle TLM 0.488189

CSS Sun-Pointing Angle 0.976378

12 July 20 @ 14:30

Pre-Burn

Thruster 1 112 8 July 20 @ 12:00

Thruster 2 112

Thruster 3 144

Thruster 4 144

Post-Burn

Thruster 1 368 12 July 20 @ 14:30

Thruster 2 368

Thruster 3 480

Thruster 4 480

Number of Pulses

Thruster 1 256

Thruster 2 256

Thruster 3 336

Thruster 4 336

Thruster Pairs

Thruster 1 & 2 512

Thruster 3 & 4 672

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430