All,

   The perigee contacts were nominal for CMD & TLM. The inertial maneuver was successful. The Orbit 534 ATS was uplinked. The SSR was dumped and the 18 day master timer was reset.

Tasks Accomplished:

CAR #1177 Orbit #534 ATS uplink

  IBEX_2021_194_o0534a_v001 93 CMDS

Reset master timer
SSR Dump -> Dump New

Set Spacecraft Time

Results from the Inertial Maneuver:

Q1 -0.55112000 ActNor.EstInrToBdy[0]

Q2 -0.01182710 ActNor.EstInrToBdy[1]

Q3 0.13360400 ActNor.EstInrToBdy[2]

Q4 0.82357600 ActNor.EstInrToBdy[3]

GPS sec 1309381933 ActNor.EstTime

UTC time 07/03/2021 21:11:59 output

MPS Diff 0.563 deg

MPS Cmd Vector X -0.170334000

MPS Cmd Vector Y 0.907633000

MPS Cmd Vector Z 0.383651000

CSS Angle TLM 1.68992

CSS Sun-Pointing Angle 3.37984

  29 June 21 @ 12:00:00

CSS Angle TLM 1.1955

CSS Sun-Pointing Angle 2.391

  03 July 21 @ 21:00:00

Pre-Burn

Thruster 1 3824 29 June 21 @ 12:00:00

Thruster 2 3760

Thruster 3 4256

Thruster 4 4320

Post-Burn

Thruster 1 4096 03 July 21 @ 21:00:00

Thruster 2 4000

Thruster 3 4528

Thruster 4 4624

Number of Pulses

Thruster 1 272

Thruster 2 240

Thruster 3 272

Thruster 4 304

Thruster Pairs 

Thruster 1 & 2 512

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