All,

   The perigee contacts were nominal for CMD and TLM. The Inertial maneuver was successful. The spacecraft looks nominal post eclipse.

Tasks Accomplished:

SSR Dump -> Dump_New & Reset Pointers

CAR 1080 Orbit 474 ATS Upload IBEX_2020_014_o0474a_V001

Reset Master Timer

Reset FDC Totals

Results from the Inertial Maneuver:

Q1 0.66888300 ActNor.EstInrToBdy[0]

Q2 0.49325400 ActNor.EstInrToBdy[1]

Q3 -0.19345000 ActNor.EstInrToBdy[2]

Q4 0.52141400 ActNor.EstInrToBdy[3]

GPS sec 1262232149 ActNor.EstTime

UTC time 01/05/2020 04:02:15 output

MPS Diff 0.782 deg

MPS Cmd Vector X 0.256390000

MPS Cmd Vector Y -0.882730000

MPS Cmd Vector Z -0.393765000

CSS Angle TLM 874469

CSS Sun-Pointing Angle 1748938

  31 Dec 19 @ 19:00

CSS Angle TLM 874469

CSS Sun-Pointing Angle 1748938

  5 Jan 20 @ 04:00

Pre-Burn

Thruster 1 1600 31 Dec 19 @ 19:00

Thruster 2 1552

Thruster 3 2208

Thruster 4 2256

Post-Burn

Thruster 1 1952 5 Jan 20 @ 04:00

Thruster 2 1904

Thruster 3 2592

Thruster 4 2640

Number of Pulses

Thruster 1 352

Thruster 2 352

Thruster 3 384

Thruster 4 384

Thruster Pairs 

Thruster 1 & 2 704

Thruster 3 & 4 768

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430