All,

    The perigee contacts were nominal. The sun maneuver was successful. The orbit 640 ATS was uplinked and the SSR was dumped.

Tasks Accomplished:

Reset Master Timer

CAR#1373 Orbit #640 ATS upload

   IBEX_2024_063_o0640a_v001 101 Commands

SSR Dump -> Dump New

Reset FDC Totals

Results from the Sun Maneuver:

CSS Angle TLM 1.23035

CSS Sun-Pointing Angle 2.4607

  18 Feb 24 @14:00:00

CSS Angle TLM 0.99426

CSS Sun-Pointing Angle 1.98852

  22 Feb 24 @21:00:00

Pre-Burn

Thruster 1 19856 18 Feb 24 @14:00:00

Thruster 2 19248

Thruster 3 26672

Thruster 4 27280

Post-Burn

Thruster 1 19936 22 Feb 24 @21:00:00

Thruster 2 19328

Thruster 3 26960

Thruster 4 27568

Number of Pulses

Thruster 1 80

Thruster 2 80

Thruster 3 288

Thruster 4 288

Thruster Pairs 

Thruster 1 & 2 160

Thruster 3 & 4 576

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

IBEX MOC (703)404-7470

Cell (301) 606-1430