All,

   The Apogee contact was nominal. The inertial was successful.

Results from the Inertial Maneuver

Q1 -0.54404300 ActNor.EstInrToBdy[0]

Q2 0.48441900 ActNor.EstInrToBdy[1]

Q3 -0.57053600 ActNor.EstInrToBdy[2]

Q4 0.37926800 ActNor.EstInrToBdy[3]

GPS sec 1330976034 ActNor.EstTime

UTC time 03/10/2022 19:33:40 output

MPS Diff 5.566 deg

MPS Cmd Vector X 0.988928000

MPS Cmd Vector Y -0.132250000

MPS Cmd Vector Z -0.067319000

CSS Angle TLM 0.900296

CSS Sun-Pointing Angle 1.800592

  06 Mar 22 @ 14:00:00

CSS Angle TLM 0.700813

CSS Sun-Pointing Angle 1.401626

  10 Mar 22 @19:30:00

Pre-Burn

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

Thruster 2 17360

Thruster 3 22608

Thruster 4 23120

Post-Burn

Thruster 1 18160 10 Mar 22 @19:30:00

Thruster 2 17648

Thruster 3 22928

Thruster 4 23440

Number of Pulses

Thruster 1 288

Thruster 2 288

Thruster 3 320

Thruster 4 320

Thruster Pairs  

Thruster 1 & 2 576

Thruster 3 & 4 640

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430