All,

   The apogee contact was nominal for CMD & TLM. The inertial maneuver was successful.

Results from the Inertial maneuver:

Q1 0.59912000 ActNor.EstInrToBdy[0]

Q2 0.24564200 ActNor.EstInrToBdy[1]

Q3 0.76204600 ActNor.EstInrToBdy[2]

Q4 0.00120183 ActNor.EstInrToBdy[3]

GPS sec 1302613326 ActNor.EstTime

UTC time 04/16/2021 13:01:52 output

MPS Diff 0.727 deg

MPS Cmd Vector X 0.910344000

MPS Cmd Vector Y 0.383590000

MPS Cmd Vector Z 0.155348000

CSS Angle TLM 0.411645

CSS Sun-Pointing Angle 0.82329

  12 Apr 21 @ 12:00:00

CSS Angle TLM 0.678108

CSS Sun-Pointing Angle 1.356216

  16 Apr 21 @ 13:00:00

Pre-Burn

Thruster 1 5232 12 Apr 21 @ 12:00:00

Thruster 2 5072

Thruster 3 6896

Thruster 4 7056

Post-Burn

Thruster 1 5504 16 Apr 21 @ 13:00:00

Thruster 2 5344

Thruster 3 7200

Thruster 4 7360

Number of Pulses

Thruster 1 272

Thruster 2 272

Thruster 3 304

Thruster 4 304

Thruster Pairs 

Thruster 1 & 2 544

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