All, 

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

 

Tasks Accomplished: 

Reset FDC Totals 

 

Results from the Inertial Maneuver: 

Q1 0.11415080 ActNor.EstInrToBdy[0] 

Q2 0.57703400 ActNor.EstInrToBdy[1] 

Q3 0.68913500 ActNor.EstInrToBdy[2] 

Q4 0.42309900 ActNor.EstInrToBdy[3] 

      

GPS sec 1336485644 ActNor.EstTime 

      

UTC time 05/13/2022 14:00:30 output 

MPS Diff 0.954 deg 

MPS Cmd Vector X 0.639493000 

MPS Cmd Vector Y 0.709283000 

MPS Cmd Vector Z 0.296592000 

CSS Angle TLM 0.613575  

CSS Sun-Pointing Angle 1.22715  

  09 May 22 @ 16:00:00 

CSS Angle TLM 0.494164  

CSS Sun-Pointing Angle 0.988328  

  13 May 22 @ 14:00:00 

Pre-Burn    

Thruster 1 1616 09 May 22 @ 16:00:00 

Thruster 2 1584  

Thruster 3 1808  

Thruster 4 1840  

Post-Burn    

Thruster 1 1856 13 May 22 @ 14:00:00 

Thruster 2 1824  

Thruster 3 2064  

Thruster 4 2096  

Number of Pulses    

Thruster 1 240  

Thruster 2 240  

Thruster 3 256  

Thruster 4 256  

Thruster Pairs   

Thruster 1 & 2 480  

Thruster 3 & 4 512