All,

    The apogee pass was nominal for CMD & TLM. The Inertial maneuver was successful.

Results from the Inertial Maneuver:

Q1 -0.47033000 ActNor.EstInrToBdy[0]

Q2 0.50817300 ActNor.EstInrToBdy[1]

Q3 -0.43591200 ActNor.EstInrToBdy[2]

Q4 0.57491800 ActNor.EstInrToBdy[3]

GPS sec 1301057985 ActNor.EstTime

UTC time 03/29/2021 12:59:31 output

MPS Diff 0.582 deg

MPS Cmd Vector X 0.993767000

MPS Cmd Vector Y 0.105852000

MPS Cmd Vector Z 0.034969000

CSS Angle TLM 0.918132

CSS Sun-Pointing Angle 1.836264

  25 Mar 21 @ 04:00:00

CSS Angle TLM 0.473953

CSS Sun-Pointing Angle 0.947906

  29 Mar 21 @ 13:00:00

Pre-Burn

Thruster 1 4112 25 Mar 21 @ 04:00:00

Thruster 2 3984

Thruster 3 5664

Thruster 4 5792

Post-Burn

Thruster 1 4394 29 Mar 21 @ 13:00:00

Thruster 2 4256

Thruster 3 5952

Thruster 4 6080

Number of Pulses

Thruster 1 282

Thruster 2 272

Thruster 3 288

Thruster 4 288

Thruster Pairs  

Thruster 1 & 2 554

Thruster 3 & 4 576

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430