All, 

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

 

Results from the Inertial Maneuver: 

Q1 -0.29792100 ActNor.EstInrToBdy[0] 

Q2 0.49018100 ActNor.EstInrToBdy[1] 

Q3 0.34701800 ActNor.EstInrToBdy[2] 

Q4 0.74198700 ActNor.EstInrToBdy[3] 

      

GPS sec 1337256067 ActNor.EstTime 

      

UTC time 05/22/2022 12:00:53 output 

 

MPS Diff 0.736 deg 

 

MPS Cmd Vector X 0.518289000 

MPS Cmd Vector Y 0.788570000 

MPS Cmd Vector Z 0.330959000 

 

CSS Angle TLM 1.73731  

CSS Sun-Pointing Angle 3.47462  

  18 May 22 @ 12:00:00 

 

CSS Angle TLM 0.28599  

CSS Sun-Pointing Angle 0.57198  

  22 May 22 @ 12:00:00 

 

Pre-Burn    

Thruster 1 2128 18 May 22 @ 12:00:00 

Thruster 2 2096  

Thruster 3 2368  

Thruster 4 2400  

Post-Burn    

Thruster 1 2384 22 May 22 @ 12:00:00 

Thruster 2 2352  

Thruster 3 2656  

Thruster 4 2688  

Number of Pulses    

Thruster 1 256  

Thruster 2 256  

Thruster 3 288          

Thruster 4 288  

Thruster Pairs   

Thruster 1 & 2 512  

Thruster 3 & 4 576