All,

    The Apogee pass was nominal for CMD & TLM. The inertial maneuver was successful. The Orbit #509 Bus and INST ATS’s have been uplinked. Timed Command count at LOS was 224.

Task’s Accomplished:

CAR 1134 ATS Upload

   IBEX_2020_332_o0509a_BUS_V001 53 cmds

   IBEX_2020_332_o0509a_INST_V001 46 cmds

Results from the Inertial Maneuver:

Q1 0.67503800 ActNor.EstInrToBdy[0]

Q2 0.44032500 ActNor.EstInrToBdy[1]

Q3 -0.57467200 ActNor.EstInrToBdy[2]

Q4 0.14208900 ActNor.EstInrToBdy[3]

GPS sec 1289537603 ActNor.EstTime

UTC time 11/16/2020 04:53:09 output

MPS Cmd Vector X -0.647603000

MPS Cmd Vector Y -0.695053000

MPS Cmd Vector Z -0.312269000

CSS Angle TLM 0.733821

CSS Sun-Pointing Angle 1.467642

  09 Nov 20 @ 14:00:00

CSS Angle TLM 1.29452

CSS Sun-Pointing Angle 2.58904

  16 Nov 20 @ 04:30:00

Pre-Burn

Thruster 1 288 09 Nov 20 @ 22:00:00

Thruster 2 256

Thruster 3 288

Thruster 4 320

Post-Burn   `

Thruster 1 576 16 Nov 20 @ 04:30:00

Thruster 2 544

Thruster 3 592

Thruster 4 624

Number of Pulses

Thruster 1 288

Thruster 2 288

Thruster 3 304

Thruster 4 304

Thruster Pairs 

Thruster 1 & 2 576

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