All, 

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

 

 

Results from the Inertial Maneuver: 

Q1 -0.60448500 ActNor.EstInrToBdy[0] 

Q2 -0.07105330 ActNor.EstInrToBdy[1] 

Q3 -0.66857700 ActNor.EstInrToBdy[2] 

Q4 0.42726400 ActNor.EstInrToBdy[3] 

      

GPS sec 1335711734 ActNor.EstTime 

      

UTC time 05/04/2022 15:02:00 output 

MPS Diff 0.267 deg 

MPS Cmd Vector X 0.748350000 

MPS Cmd Vector Y 0.612495000 

MPS Cmd Vector Z 0.254602000 

CSS Angle TLM 1.73068  

CSS Sun-Pointing Angle 3.46136  

  30 Apr 22 @ 14:30:00 

CSS Angle TLM 0.659975  

CSS Sun-Pointing Angle 1.31995  

  04 May 22 @ 15:00:00 

Pre-Burn    

Thruster 1 1072 30 Apr 22 @ 14:30:00 

Thruster 2 1072  

Thruster 3 1184  

Thruster 4 1184  

Post-Burn    

Thruster 1 1360 04 May 22 @ 15:00:00 

Thruster 2 1328  

Thruster 3 1520  

Thruster 4 1552  

Number of Pulses    

Thruster 1 288  

Thruster 2 256  

Thruster 3 336  

Thruster 4 368  

Thruster Pairs   

Thruster 1 & 2 544  

Thruster 3 & 4 704