All, 

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

 

Tasks Accomplished: 

Reset FDC Totals 

 

Results from the Inertial Maneuver: 

Q1 0.33876900 ActNor.EstInrToBdy[0] 

Q2 -0.49448600 ActNor.EstInrToBdy[1] 

Q3 -0.77840800 ActNor.EstInrToBdy[2] 

Q4 0.18655000 ActNor.EstInrToBdy[3] 

      

GPS sec 1344218427 ActNor.EstTime 

UTC time 08/11/2022 02:00:13 output 

 

MPS Diff 0.878 deg 

 

MPS Cmd Vector X -0.718260000 

MPS Cmd Vector Y 0.642266000 

MPS Cmd Vector Z 0.267575000 

 

CSS Angle TLM 2.01295  

CSS Sun-Pointing Angle 4.0259  

  06 Aug 22 @11:30:00 

 

CSS Angle TLM 0.454134  

CSS Sun-Pointing Angle 0.908268  

  11 Aug 22 @02:00:00 

 

Pre-Burn    

Thruster 1 3616 06 Aug 22 @11:30:00 

Thruster 2 3520  

Thruster 3 4144  

Thruster 4 4240  

Post-Burn    

Thruster 1 3888 11 Aug 22 @02:00:00 

Thruster 2 3792  

Thruster 3 4416  

Thruster 4 4512  

Number of Pulses    

Thruster 1 272  

Thruster 2 272  

Thruster 3 272  

Thruster 4 272  

Thruster Pairs   

Thruster 1 & 2 544  

Thruster 3 & 4 544