All,

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

Results from the Inertial Maneuver:

Q1 0.78252900 ActNor.EstInrToBdy[0]

Q2 -0.28106100 ActNor.EstInrToBdy[1]

Q3 0.33090300 ActNor.EstInrToBdy[2]

Q4 0.44627000 ActNor.EstInrToBdy[3]

GPS sec 1325350825 ActNor.EstTime

UTC time 01/04/2022 17:00:11 output

MPS Diff 0.661 deg

MPS Cmd Vector X 0.272934000

MPS Cmd Vector Y -0.878990000

MPS Cmd Vector Z -0.391004000

CSS Angle TLM 0.815894

CSS Sun-Pointing Angle 1.631788

  31 Dec 21 @ 14:00:00

CSS Angle TLM 0.844415

CSS Sun-Pointing Angle 1.68883

  04 Jan 22 @ 17:00:00

Pre-Burn

Thruster 1 14240 31 Dec 21 @ 14:00:00

Thruster 2 13856

Thruster 3 17776

Thruster 4 18160

Post-Burn

Thruster 1 14528 04 Jan 22 @ 17:00:00

Thruster 2 14144

Thruster 3 18080

Thruster 4 18464

Number of Pulses

Thruster 1 288

Thruster 2 288

Thruster 3 304

Thruster 4 304

Thruster Pairs  

Thruster 1 & 2 576

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