All,

    The perigee contacts were nominal. The inertial maneuver was successful. The Orbit 547 ATS was uplinked. The ssr was dumped. The 18 day timer and FDC totals were reset.

Tasks Accomplished:

Clear FDC totals

Reset 18 Day Timer

CAR # 1201 Orbit 547 ATS uplink

    IBEX_2021_310_o0547a_v001 91 cmds

SSR Dump -> Dump New

Set the Spacecraft Clock

Results from the Inertial Maneuver:

Q1 -0.44861300 ActNor.EstInrToBdy[0]

Q2 -0.63890600 ActNor.EstInrToBdy[1]

Q3 0.57129900 ActNor.EstInrToBdy[2]

Q4 0.25330400 ActNor.EstInrToBdy[3]

GPS sec 1319521074 ActNor.EstTime

UTC time 10/29/2021 05:37:40 output

MPS Diff 0.500 deg

MPS Cmd Vector X -0.837958000

MPS Cmd Vector Y -0.497069000

MPS Cmd Vector Z -0.225274000

CSS Angle TLM 0.653719

CSS Sun-Pointing Angle 1.307438

  25 Oct 21 @ 23:00:00

CSS Angle TLM 0.531923

CSS Sun-Pointing Angle 1.063846

  28 Oct 21 @ 15:00:00

Pre-Burn

Thruster 1 10384 25 Oct 21 @ 23:00:00

Thruster 2 10112

Thruster 3 12640

Thruster 4 12912

Post-Burn

Thruster 1 10480 28 Oct 21 @ 15:00:00

Thruster 2 10208

Thruster 3 12800

Thruster 4 13072

Number of Pulses

Thruster 1 96

Thruster 2 96

Thruster 3 160

Thruster 4 160

Thruster Pairs  

Thruster 1 & 2 192

Thruster 3 & 4 320

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430