All,

   The contact was nominal for CMD and TLM. The Apogee Inertial maneuver was successful.

The ATS “IBEX_2020_078_o0481a_v002” was uplinked.

Results from the maneuver

Q1 0.15842300 ActNor.EstInrToBdy[0]

Q2 0.70537900 ActNor.EstInrToBdy[1]

Q3 0.07675550 ActNor.EstInrToBdy[2]

Q4 0.68662300 ActNor.EstInrToBdy[3]

GPS sec 1268421348 ActNor.EstTime

MPS Diff 0.696 deg

MPS Cmd Vector X 0.992482000

MPS Cmd Vector Y -0.108116000

MPS Cmd Vector Z -0.057355000

CSS Angle TLM 0.790063

CSS Sun-Pointing Angle 1.580126

  09 Mar 20 @ 05:00

CSS Angle TLM 0.678397

CSS Sun-Pointing Angle 1.356794

  16 Mar 20 @ 19:00

Pre-Burn

Thruster 1 5392 09 Mar 20 @ 05:00

Thruster 2 5248

Thruster 3 7376

Thruster 4 7520

Post-Burn

Thruster 1 5680 16 Mar 20 @ 19:00

Thruster 2 5488

Thruster 3 7696

Thruster 4 7888

Number of Pulses

Thruster 1 288

Thruster 2 240

Thruster 3 320

Thruster 4 368

Thruster Pairs 

Thruster 1 & 2 528

Thruster 3 & 4 688

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430