All,

   The Perigee passes were nominal for CMD and TLM. The Inertial maneuver was successful.

The following was accomplished:

SSR Dump -> Dump New

Reset Master Timer

CAR # 1072 Upload Orbit #468 Lo Gain Cal ATS

CAR # 1073 Dump Orbit # 466 Missing Blocks

Results from the Inertial maneuver:

Q1 0.72034700 ActNor.EstInrToBdy[0]

Q2 0.37370900 ActNor.EstInrToBdy[1]

Q3 -0.53247100 ActNor.EstInrToBdy[2]

Q4 0.24065800 ActNor.EstInrToBdy[3]

GPS sec 1258237910 ActNor.EstTime

MPS Diff 0.837 deg

MPS Cmd Vector X -0.584749000

MPS Cmd Vector Y -0.740660000

MPS Cmd Vector Z -0.330893000

CSS Angle TLM 0.666466

CSS Sun-Pointing Angle 1.332932

  17 Nov 19 @ 00:30

CSS Angle TLM 0.711894

CSS Sun-Pointing Angle 1.423788

  19 Nov 19 @ 22:30

Pre-Burn

Thruster 1 20352 10 Nov 19 @ 06:00

Thruster 2 19728

Thruster 3 26448

Thruster 4 27072

Post-Burn

Thruster 1 20784 19 Nov 19 @ 22:30

Thruster 2 20160

Thruster 3 27152

Thruster 4 27776

Number of Pulses

Thruster 1 432

Thruster 2 432

Thruster 3 704

Thruster 4 704

Thruster Pairs 

Thruster 1 & 2 864

Thruster 3 & 4 1408

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430