All,

   The spacecraft looks nominal post penumbra eclipse. Battery voltages and temperature are nominal. The inertial maneuver was successful. During the pass the FDC totals were reset to zero. 

Task’s accomplished:

Reset FDC Totals

Results from the inertial Maneuver:

Q1 -0.53730500 ActNor.EstInrToBdy[0]

Q2 -0.13342800 ActNor.EstInrToBdy[1]

Q3 -0.38492900 ActNor.EstInrToBdy[2]

Q4 0.73846500 ActNor.EstInrToBdy[3]

GPS sec 1307444539 ActNor.EstTime

UTC time 06/11/2021 11:02:05 output

MPS Cmd Vector X 0.209806000

MPS Cmd Vector Y 0.901019000

MPS Cmd Vector Z 0.379666000

MPS Diff 0.633 deg

CSS Angle TLM 0.362077

CSS Sun-Pointing Angle 0.724154

07 June 21 @ 00:30:00

CSS Angle TLM 0.415901

CSS Sun-Pointing Angle 0.831802

11 June 21 @ 11:00:00

Pre-Burn

Thruster 1 2512 07 June 21 @ 00:30:00

Thruster 2 2480

Thruster 3 2672

Thruster 4 2704

Post-Burn

Thruster 1 2784 11 June 21 @ 11:00:00

Thruster 2 2752

Thruster 3 2960

Thruster 4 2992

Number of Pulses

Thruster 1 272

Thruster 2 272

Thruster 3 288

Thruster 4 288

Thruster Pairs

Thruster 1 & 2 544

Thruster 3 & 4 576

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430