All, 

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

 

 

Results from the Inertial Maneuver: 

Q1 -0.63128600 ActNor.EstInrToBdy[0] 

Q2 0.10733100 ActNor.EstInrToBdy[1] 

Q3 0.74268900 ActNor.EstInrToBdy[2] 

Q4 0.19588800 ActNor.EstInrToBdy[3] 

      

GPS sec 1345858305 ActNor.EstTime 

UTC time 08/30/2022 01:31:31 output 

 

MPS Diff 0.761 deg 

 

MPS Cmd Vector X -0.896243000 

MPS Cmd Vector Y 0.410824000 

MPS Cmd Vector Z 0.167251000 

 

CSS Angle TLM 0.578107  

CSS Sun-Pointing Angle 1.156214  

  25 Aug 22 @13:00:00 

 

CSS Angle TLM 0.773077  

CSS Sun-Pointing Angle 1.546154  

  30 Aug 22 @01:00:00 

 

Pre-Burn    

Thruster 1 4720 25 Aug 22 @13:00:00 

Thruster 2 4624  

Thruster 3 5328  

Thruster 4 5424  

Post-Burn    

Thruster 1 5024 30 Aug 22 @01:00:00 

Thruster 2 4896  

Thruster 3 5648  

Thruster 4 5776  

Number of Pulses    

Thruster 1 304  

Thruster 2 272  

Thruster 3 320  

Thruster 4 352  

Thruster Pairs   

Thruster 1 & 2 576  

Thruster 3 & 4 672