All,

    The apogee pass was nominal for CMD & TLM. The Inertial maneuver was successful.

Results from the Inertial Maneuver:

Q1 -0.64059000 ActNor.EstInrToBdy[0]

Q2 0.35618300 ActNor.EstInrToBdy[1]

Q3 -0.64153600 ActNor.EstInrToBdy[2]

Q4 0.22629700 ActNor.EstInrToBdy[3]

GPS sec 1299434529 ActNor.EstTime

UTC time 03/10/2021 18:01:55 output

MPS Diff 0.659 deg

MPS Cmd Vector X 0.984615000

MPS Cmd Vector Y -0.156282000

MPS Cmd Vector Z -0.078163000

CSS Angle TLM 0.95121

CSS Sun-Pointing Angle 1.90242

  6 Mar 21 @ 11:00:00

CSS Angle TLM 1.35292

CSS Sun-Pointing Angle 2.70584

  10 Mar 21 @ 18:00:00

Pre-Burn

Thruster 1 3248 6 Mar 21 @ 11:00:00

Thruster 2 3120

Thruster 3 4640

Thruster 4 4768

Post-Burn

Thruster 1 3392 10 Mar 21 @ 18:00:00

Thruster 2 3264

Thruster 3 4800

Thruster 4 4928

Number of Pulses

Thruster 1 144

Thruster 2 144

Thruster 3 160

Thruster 4 160

Thruster Pairs 

Thruster 1 & 2 288

Thruster 3 & 4 320

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430