All,

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

 

Results from the Inertial Maneuver>:

Q1 0.63348400 ActNor.EstInrToBdy[0]

Q2 0.29693700 ActNor.EstInrToBdy[1]

Q3 0.66084200 ActNor.EstInrToBdy[2]

Q4 0.27168900 ActNor.EstInrToBdy[3]

     

GPS sec 1363867269 ActNor.EstTime

UTC time 03/26/2023 12:00:55 output

 

MPS Diff 0.596 deg

MPS Cmd Vector X 0.998419000

MPS Cmd Vector Y 0.054719000

MPS Cmd Vector Z 0.012880000

 

CSS Angle TLM 0.836031

CSS Sun-Pointing Angle 1.672062

  22 Mar 23@10:00:00

 

CSS Angle TLM 0.343781

CSS Sun-Pointing Angle 0.687562

  26 Mar 23@12:00:00

 

Pre-Burn   

Thruster 1 1842 22 Mar 23@10:00:00

Thruster 2 1744

Thruster 3 2000

Thruster 4 2080

Post-Burn  

Thruster 1 2016 26 Mar 23@12:00:00

Thruster 2 1936

Thruster 3 2224

Thruster 4 2304

Number of Pulses  

Thruster 1 174

Thruster 2 192

Thruster 3 224

Thruster 4 224

Thruster Pairs  

Thruster 1 & 2 366

Thruster 3 & 4 448