All,

The perigee contacts were nominal for CMD & TLM. The Inertial maneuver was successful.

The following was accomplished:

SSR Dump -> Dump New

Reset Master Timer

Set Spacecraft Clock

Reset FDC Totals

Results from the Inertial maneuver:

Q1 0.43030900 ActNor.EstInrToBdy[0]

Q2 -0.47554900 ActNor.EstInrToBdy[1]

Q3 -0.70310300 ActNor.EstInrToBdy[2]

Q4 0.30713700 ActNor.EstInrToBdy[3]

GPS sec 1251201617 ActNor.EstTime

UTC time 08/30/2019 12:00:03 output

MPS Cmd Vector X -0.898903000

MPS Cmd Vector Y 0.405493000

MPS Cmd Vector Z 0.165977000

MPS Diff 0.664 deg

CSS Angle TLM 0.360452

CSS Sun-Pointing Angle 0.720904

25 Aug 19 @ 10:30

CSS Angle TLM 0.336882

CSS Sun-Pointing Angle 0.673764

30 Aug 19 @ 12:00

Pre-Burn

Thruster 1 17056 25 Aug 19 @ 10:30

Thruster 2 16608

Thruster 3 20128

Thruster 4 20576

Post-Burn

Thruster 1 17312 30 Aug 19 @ 12:00

Thruster 2 16864

Thruster 3 20416

Thruster 4 20864

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

tim.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430

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