All,

   The Apogee contact was nominal for CMD and TLM. The Inertial maneuver was successful. The FDC totals were reset during the pass.

Results from the Maneuver:  

0.79539700 ActNor.EstInrToBdy[0]

0.01576120 ActNor.EstInrToBdy[1]

0.45585700 ActNor.EstInrToBdy[2]

0.39911100 ActNor.EstInrToBdy[3]

GPS sec 1265043626 ActNor.EstTime

UTC time 02/06/2020 17:00:12 output

MPS Diff 0.789 deg

MPS Cmd Vector X 0.742163000

MPS Cmd Vector Y -0.611226000

MPS Cmd Vector Z -0.274949000

CSS Angle TLM 1.03628

CSS Sun-Pointing Angle 2.07256

  01 Feb 20 @ 16:00

CSS Angle TLM 1.16718

CSS Sun-Pointing Angle 2.33436

  06 Feb 20 @ 17:00

Pre-Burn

Thruster 1 3408 01 Feb 20 @ 16:00

Thruster 2 3312

Thruster 3 4768

Thruster 4 4864

Post-Burn

Thruster 1 3680 06 Feb 20 @ 17:00

Thruster 2 3584

Thruster 3 5072

Thruster 4 5168

Number of Pulses

Thruster 1 272

Thruster 2 272

Thruster 3 304

Thruster 4 304

Thruster Pairs 

Thruster 1 & 2 544

Thruster 3 & 4 608

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430