All, 

   The apogee contact was nominal. The sun maneuver was successful. During the contact I was able to set the static Z rate. The Static Z rate was changed from 4.182 to 4.164.  

 

 

Results from the Sun Maneuver: 

CSS Angle TLM 0.905038  

CSS Sun-Pointing Angle 1.810076  

  10 Oct 22 @14:30:00 

CSS Angle TLM 1.79275  

CSS Sun-Pointing Angle 3.5855  

  17 Oct 22 @00:30:00 

Pre-Burn    

Thruster 1 7248 10 Oct 22 @14:30:00 

Thruster 2 7056  

Thruster 3 8960  

Thruster 4 9152  

Post-Burn    

Thruster 1 7488 17 Oct 22 @00:30:00 

Thruster 2 7248  

Thruster 3 9392  

Thruster 4 9632  

Number of Pulses 9632  

Thruster 1 240  

Thruster 2 192  

Thruster 3 432  

Thruster 4 480  

Thruster Pairs   

Thruster 1 & 2 432  

Thruster 3 & 4 912