All,

  The Apogee contact was nominal. The inertial maneuver was successful.

Tasks Accomplished:

Reset FDC Totals

Results from Inertial Maneuver:

Q1 0.74981900 ActNor.EstInrToBdy[0]

Q2 -0.00577635 ActNor.EstInrToBdy[1]

Q3 0.63484400 ActNor.EstInrToBdy[2]

Q4 0.18631000 ActNor.EstInrToBdy[3]

GPS sec 1330264823 ActNor.EstTime

UTC time 03/02/2022 14:00:09 output

MPS Diff 0.681 deg

MPS Cmd Vector X 0.952271000

MPS Cmd Vector Y -0.276300000

MPS Cmd Vector Z -0.129765000

CSS Angle TLM 1.9

CSS Sun-Pointing Angle 3.8

  25 Feb 22 @ 07:00:00

CSS Angle TLM 0.861846

CSS Sun-Pointing Angle 1.723692

  02 Mar 22 @ 14:00:00

Pre-Burn

Thruster 1 17344 25 Feb 22 @ 07:00:00

Thruster 2 16832

Thruster 3 22000

Thruster 4 22512

Post-Burn

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

Thruster 2 17088

Thruster 3 22304

Thruster 4 22816

Number of Pulses

Thruster 1 256

Thruster 2 256

Thruster 3 304

Thruster 4 304

Thruster Pairs  

Thruster 1 & 2 512

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