All, 

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

 

 

Results from the Inertial Maneuver 

:Q1 -0.20813700 ActNor.EstInrToBdy[0] 

Q2 -0.50738600 ActNor.EstInrToBdy[1] 

Q3 -0.75758900 ActNor.EstInrToBdy[2] 

Q4 0.35397500 ActNor.EstInrToBdy[3] 

      

GPS sec 1340359204 ActNor.EstTime 

UTC time 06/27/2022 09:59:50 output 

MPS Diff 0.748 deg 

MPS Cmd Vector X -0.050644000 

MPS Cmd Vector Y 0.920241000 

MPS Cmd Vector Z 0.388063000 

CSS Angle TLM 0.49218  

CSS Sun-Pointing Angle 0.98436  

  22 June 22 @15:00:00 

CSS Angle TLM 0.656706  

CSS Sun-Pointing Angle 1.313412  

  27 June 22 @10:00:00 

Pre-Burn    

Thruster 1 928 22 June 22 @15:00:00 

Thruster 2 896  

Thruster 3 1264  

Thruster 4 1296  

Post-Burn    

Thruster 1 1184 27 June 22 @10:00:00 

Thruster 2 1152  

Thruster 3 1552  

Thruster 4 1584  

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