All, 

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

 

Results from the Inertial Maneuver: 

Q1 -0.30546800 ActNor.EstInrToBdy[0] 

Q2 0.45864600 ActNor.EstInrToBdy[1] 

Q3 0.77521800 ActNor.EstInrToBdy[2] 

Q4 0.30882100 ActNor.EstInrToBdy[3] 

      

GPS sec 1341143987 ActNor.EstTime 

      

UTC time 07/06/2022 11:59:33 output 

MPS Diff 0.852 deg 

MPS Cmd Vector X -0.198474000 

MPS Cmd Vector Y 0.903162000 

MPS Cmd Vector Z 0.380667000 

CSS Angle TLM 0.298707  

CSS Sun-Pointing Angle 0.597414  

  01 July 22 @10:00:00 

CSS Angle TLM 0.3743  

CSS Sun-Pointing Angle 0.7486  

  06 July 22 @15:00:00 

Pre-Burn    

Thruster 1 1456 01 July 22 @10:00:00 

Thruster 2 1424  

Thruster 3 1872  

Thruster 4 1904  

Post-Burn    

Thruster 1 1680 06 July 22 @15:00:00 

Thruster 2 1648  

Thruster 3 2128  

Thruster 4 2160  

Number of Pulses    

Thruster 1 224  

Thruster 2 224  

Thruster 3 256  

Thruster 4 256  

Thruster Pairs   

Thruster 1 & 2 448  

Thruster 3 & 4 512