All, 

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

 

Results from the Inertial Maneuver: 

Q1 -0.56674700 ActNor.EstInrToBdy[0] 

Q2 -0.06300950 ActNor.EstInrToBdy[1] 

Q3 0.33844900 ActNor.EstInrToBdy[2] 

Q4 0.74851800 ActNor.EstInrToBdy[3] 

      

GPS sec 1342692123 ActNor.EstTime    

UTC time 07/24/2022 10:01:49 output 

 

MPS Diff 0.590 deg 

 

MPS Cmd Vector X -0.478457000 

MPS Cmd Vector Y 0.809574000 

MPS Cmd Vector Z 0.340101000 

 

CSS Angle TLM 0.27052  

CSS Sun-Pointing Angle 0.54104  

  19 July 22 @19:30:00 

 

CSS Angle TLM 0.111906  

CSS Sun-Pointing Angle 0.223812  

  24 July 22 @10:00:00 

 

Pre-Burn    

Thruster 1 2512 19 July 22 @19:30:00 

Thruster 2 2448  

Thruster 3 2992  

Thruster 4 3056  

Post-Burn    

Thruster 1 2784 24 July 22 @10:00:00 

Thruster 2 2720  

Thruster 3 3296  

Thruster 4 3360  

Number of Pulses    

Thruster 1 272  

Thruster 2 272  

Thruster 3 304  

Thruster 4 304  

Thruster Pairs   

Thruster 1 & 2 544  

Thruster 3 & 4 608