All,

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

Results from the Inertial Maneuver:

Q1 -0.12193900 ActNor.EstInrToBdy[0]

Q2 0.70317400 ActNor.EstInrToBdy[1]

Q3 -0.15192300 ActNor.EstInrToBdy[2]

Q4 0.68381000 ActNor.EstInrToBdy[3]

GPS sec 1300280633 ActNor.EstTime

UTC time 03/20/2021 13:03:39 output

MPS Cmd Vector X 0.998830000

MPS Cmd Vector Y -0.039419000

MPS Cmd Vector Z -0.028009000

MPS Diff 0.687 deg

CSS Angle TLM 0.512819

CSS Sun-Pointing Angle 1.025638

  16 Mar 21 @ 03:30:00

CSS Angle TLM 0.582491

CSS Sun-Pointing Angle 1.164982

  20 Mar 21 @ 13:00:00

Pre-Burn

Thruster 1 3552 16 Mar 21 @ 03:30:00

Thruster 2 3424

Thruster 3 5008

Thruster 4 5136

Post-Burn

Thruster 1 3840 20 Mar 21 @ 13:00:00

Thruster 2 3712

Thruster 3 5328

Thruster 4 5456

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