All,

    The apogee contact was nominal, and the sun maneuver was successful. The Star tracker percent valid was at 77%, so I was able to set the static z rate.

 

Tasks Accomplished:

Reset FDC Totals

Set Static Z Rate 4.174 – 4.179

 

Results from the Sun Maneuver:

CSS Angle TLM 1.31

CSS Sun-Pointing Angle 2.62

  29 Dec 23 @23:30:00

CSS Angle TLM 0.376385

CSS Sun-Pointing Angle 0.75277

  04 Jan 24 @18:00:00

Pre-Burn   

Thruster 1 17200 29 Dec 23 @23:30:00

Thruster 2 16688

Thruster 3 22672

Thruster 4 23184

Post-Burn  

Thruster 1 17312 04 Jan 24 @18:00:00

Thruster 2 16800

Thruster 3 23008

Thruster 4 23520

Number of Pulses  

Thruster 1 112

Thruster 2 112

Thruster 3 336

Thruster 4 336

Thruster Pairs  

Thruster 1 & 2 224

Thruster 3 & 4 672

 

 

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