All, 

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

 

Results from the Inertial Maneuver: 

Q1 -0.40091600 ActNor.EstInrToBdy[0] 

Q2 0.39394800 ActNor.EstInrToBdy[1] 

Q3 0.28048100 ActNor.EstInrToBdy[2] 

Q4 0.77807600 ActNor.EstInrToBdy[3] 

      

GPS sec 1338037345 ActNor.EstTime 

UTC time 05/31/2022 13:02:11 output 

 

MPS Diff 0.702 deg 

 

MPS Cmd Vector X 0.384969000 

MPS Cmd Vector Y 0.850711000 

MPS Cmd Vector Z 0.357895000 

 

CSS Angle TLM 0.351102  

CSS Sun-Pointing Angle 0.702204  

  26 May 22 @ 20:00:00 

 

CSS Angle TLM 0.148038  

CSS Sun-Pointing Angle 0.296076  

  31 May 22 @ 13:00:00 

 

Pre-Burn    

Thruster 1 2640 26 May 22 @ 20:00:00 

Thruster 2 2608  

Thruster 3 2976  

Thruster 4 3008  

Post-Burn    

Thruster 1 2896 31 May 22 @ 13:00:00 

Thruster 2 2864  

Thruster 3 3248  

Thruster 4 3280  

Number of Pulses    

Thruster 1 256  

Thruster 2 256  

Thruster 3 272  

Thruster 4 272  

Thruster Pairs   

Thruster 1 & 2 512  

Thruster 3 & 4 544