All,

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

Results from the Inertial maneuver:

Q1 0.58797200 ActNor.EstInrToBdy[0]

Q2 0.45187000 ActNor.EstInrToBdy[1]

Q3 0.42428700 ActNor.EstInrToBdy[2]

Q4 0.51969500 ActNor.EstInrToBdy[3]

GPS sec 1267642866 ActNor.EstTime

UTC time 03/07/2020 19:00:52 output

MPS Diff 0.468 deg

MPS Cmd Vector X 0.968514000

MPS Cmd Vector Y -0.224614000

MPS Cmd Vector Z -0.107375000

CSS Angle TLM 0.696893

CSS Sun-Pointing Angle 1.393786

  29 Feb 20 @ 00:05

CSS Angle TLM 0.869307

CSS Sun-Pointing Angle 1.738614

  07 Mar 20 @ 00:05

Pre-Burn

Thruster 1 5040 29 Feb 20 @ 00:05

Thruster 2 4896

Thruster 3 6704

Thruster 4 6848

Post-Burn

Thruster 1 5328 07 Mar 20 @ 00:05

Thruster 2 5184

Thruster 3 7056

Thruster 4 7200

Number of Pulses

Thruster 1 288

Thruster 2 288

Thruster 3 352

Thruster 4 352

Thruster Pairs 

Thruster 1 & 2 576

Thruster 3 & 4 704

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430