All,

   The contact was nominal and the inertial maneuver was successful.

Results from the inertial maneuver:

Q1 0.37699700 ActNor.EstInrToBdy[0]

Q2 0.60106400 ActNor.EstInrToBdy[1]

Q3 0.36030300 ActNor.EstInrToBdy[2]

Q4 0.60562100 ActNor.EstInrToBdy[3]

GPS sec 1331813014 ActNor.EstTime

UTC time 03/20/2022 12:03:20 output

MPS Diff 0.822 deg

MPS Cmd Vector X 0.999799000

MPS Cmd Vector Y -0.012338000

MPS Cmd Vector Z -0.015795000

CSS Angle TLM 0.99426

CSS Sun-Pointing Angle 1.98852

  16 Mar 22 @02:00:00

CSS Angle TLM 0.867779

CSS Sun-Pointing Angle 1.735558

  20 Mar 22 @12:00:00

Pre-Burn

Thruster 1 18256 16 Mar 22 @02:00:00

Thruster 2 17744

Thruster 3 23296

Thruster 4 23808

Post-Burn

Thruster 1 18496 20 Mar 22 @12:00:00

Thruster 2 17984

Thruster 3 23552

Thruster 4 24064

Number of Pulses

Thruster 1 240

Thruster 2 240

Thruster 3 256

Thruster 4 256

Thruster Pairs  

Thruster 1 & 2 480

Thruster 3 & 4 512

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430