All,

   The Apogee contact was nominal for CMD and TLM. The Inertial maneuver was successful.

Results from the Inertial maneuver:

Q1 -0.50338100 ActNor.EstInrToBdy[0]

Q2 0.25270700 ActNor.EstInrToBdy[1]

Q3 0.64557300 ActNor.EstInrToBdy[2]

Q4 0.51573400 ActNor.EstInrToBdy[3]

GPS sec 1279022640 ActNor.EstTime

UTC time 07/17/2020 12:03:46 output

MPS Diff 0.532 deg

MPS Cmd Vector X -0.387384000

MPS Cmd Vector Y 0.849800000

MPS Cmd Vector Z 0.357455000

CSS Angle TLM 0.488189

CSS Sun-Pointing Angle 0.976378

  12 July 20 @ 14:30

CSS Angle TLM 0.0862292

CSS Sun-Pointing Angle 0.1724584

  12 July 20 @ 14:30

Pre-Burn

Thruster 1 368 12 July 20 @ 14:30

Thruster 2 368

Thruster 3 480

Thruster 4 480

Post-Burn

Thruster 1 656 12 July 20 @ 14:30

Thruster 2 624

Thruster 3 800

Thruster 4 832

Number of Pulses

Thruster 1 288

Thruster 2 256

Thruster 3 320

Thruster 4 352

Thruster Pairs 

Thruster 1 & 2 544

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