All,

    The apogee contact was nominal. The sun maneuver was successful. At AOS the STA Percent Valid was 63 and I was able to set the static z rate. The static z rate was changed from 4.172 -> 4.179.  

 

Tasks Accomplished:

Set Static Z rate

 

Results from the Sun Maneuver:

CSS Angle TLM 1.07865

CSS Sun-Pointing Angle 2.1573

  16 Nov 22@06:00:00

CSS Angle TLM 0.979587

CSS Sun-Pointing Angle 1.959174

  21 Nov 22@20:00:00

Pre-Burn   

Thruster 1 288 16 Nov 22@06:00:00

Thruster 2 288

Thruster 3 336

Thruster 4 336

Post-Burn  

Thruster 1 640 21 Nov 22@20:00:00

Thruster 2 640

Thruster 3 912

Thruster 4 912

Number of Pulses  

Thruster 1 352

Thruster 2 352

Thruster 3 576

Thruster 4 576

Thruster Pairs  

Thruster 1 & 2 704

Thruster 3 & 4 1152