All,

    The perigee contacts were nominal for CMD and TLM. The inertial maneuver was successful. The 18 day timer was reset. The spacecraft clock was set and orbit 561 ATS was uplinked.

        Tim

Tasks Accomplished:

  Set Spacecraft clock

  Reset 18 Day Timer

  CAR 1230 Orbit #561 ATS upload

  SSR dump -> Dump New

  Reset FDC Totals

Results from the Inertial Maneuver:

Q1 0.62935500 ActNor.EstInrToBdy[0]

Q2 0.38778800 ActNor.EstInrToBdy[1]

Q3 0.48198300 ActNor.EstInrToBdy[2]

Q4 0.47034600 ActNor.EstInrToBdy[3]

GPS sec 1330610440 ActNor.EstTime

UTC time 03/06/2022 14:00:26 output

MPS Diff 0.806 deg

MPS Cmd Vector X 0.973273000

MPS Cmd Vector Y -0.206485000

MPS Cmd Vector Z -0.100518000

CSS Angle TLM 0.861846

CSS Sun-Pointing Angle 1.723692

  02 Mar 22 @ 14:00:00

CSS Angle TLM 0.900296

CSS Sun-Pointing Angle 1.800592

  06 Mar 22 @ 14:00:00

Pre-Burn

Thruster 1 17600 02 Mar 22 @ 14:00:00

Thruster 2 17088

Thruster 3 22304

Thruster 4 22816

Post-Burn

Thruster 1 17872 06 Mar 22 @ 14:00:00

Thruster 2 17360

Thruster 3 22608

Thruster 4 23120

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