All, 

   The apogee contact was nominal and the Inertial maneuver was successful. 

 

 

Results from the Inertial Maneuver: 

Q1 -0.51949600 ActNor.EstInrToBdy[0] 

Q2 -0.18173800 ActNor.EstInrToBdy[1] 

Q3 -0.36336400 ActNor.EstInrToBdy[2] 

Q4 0.75170600 ActNor.EstInrToBdy[3] 

      

GPS sec 1339588849 ActNor.EstTime 

      

UTC time 06/18/2022 12:00:35 output 

 

MPS Diff 0.595 

 

MPS Cmd Vector X 0.098240000 

MPS Cmd Vector Y 0.916981000 

MPS Cmd Vector Z 0.386647000 

 

CSS Angle TLM 1.60279  

CSS Sun-Pointing Angle 3.20558  

  13 June 22 @17:00:00 

 

CSS Angle TLM 0.263167  

CSS Sun-Pointing Angle 0.526334  

  18 June 22 @12:00:00 

 

Pre-Burn    

Thruster 1 528 13 June 22 @17:00:00 

Thruster 2 528  

Thruster 3 848  

Thruster 4 848  

Post-Burn    

Thruster 1 656 18 June 22 @12:00:00 

Thruster 2 624  

Thruster 3 976  

Thruster 4 1008  

Number of Pulses    

Thruster 1 128  

Thruster 2 96  

Thruster 3 128  

Thruster 4 160  

Thruster Pairs   

Thruster 1 & 2 224  

Thruster 3 & 4 288