All,

    The apogee contact was nominal. The sun maneuver was successful.

 

 

 

Results from the Sun Maneuver:

CSS Angle TLM 0.237388

CSS Sun-Pointing Angle 0.474776

  01 Oct 22 @05:00:00

CSS Angle TLM 1.9069

CSS Sun-Pointing Angle 3.8138

  06 Oct 22 @23:30:00

Pre-Burn   

Thruster 1 6752 01 Oct 22 @05:00:00

Thruster 2 6592

Thruster 3 7936

Thruster 4 8096

Post-Burn  

Thruster 1 7120 06 Oct 22 @23:30:00

Thruster 2 6928

Thruster 3 8576

Thruster 4 8768

Number of Pulses  

Thruster 1 368

Thruster 2 336

Thruster 3 640

Thruster 4 672

Thruster Pairs  

Thruster 1 & 2 704

Thruster 3 & 4 1312

 

 

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430