All, 

   The apogee contact was nominal. The inertial maneuver was successful. The Orbit 563 ATS was uplinked. 

 

Tasks Accomplished: 

Reset FDC Totals 

CAR 1234 Orbit #563 ATS uplink 

    IBEX _2022_093_o0563a_v001 93 cmds 

 

 

Results from the Inertial Maneuver: 

Q1 -0.04821150 ActNor.EstInrToBdy[0] 

Q2 0.68997500 ActNor.EstInrToBdy[1] 

Q3 0.01905210 ActNor.EstInrToBdy[2] 

Q4 0.72197500 ActNor.EstInrToBdy[3] 

      

GPS sec 1332597776 ActNor.EstTime 

      

UTC time 03/29/2022 14:02:42 output 

MPS Diff 0.668 deg 

MPS Cmd Vector X 0.994210000 

MPS Cmd Vector Y 0.102145000 

MPS Cmd Vector Z 0.033365000 

CSS Angle TLM 0.370623  

CSS Sun-Pointing Angle 0.741246  

  25 Mar 22 @03:00:00 

CSS Angle TLM 0.310274  

CSS Sun-Pointing Angle 0.620548  

  29 Mar 22 @14:00:00 

Pre-Burn    

Thruster 1 18656 25 Mar 22 @03:00:00 

Thruster 2 18144  

Thruster 3 23776  

Thruster 4 24288  

Post-Burn    

Thruster 1 18960 29 Mar 22 @14:00:00 

Thruster 2 18400  

Thruster 3 24064  

Thruster 4 24624  

Number of Pulses    

Thruster 1 304  

Thruster 2 256  

Thruster 3 288  

Thruster 4 336  

Thruster Pairs   

Thruster 1 & 2 560  

Thruster 3 & 4 624