All,

The Orbit# 490 Apogee Contact was nominal for command/telemetry.

 

Q1          -0.14920100        ActNor.EstInrToBdy[0]

Q2          0.53152300          ActNor.EstInrToBdy[1]

Q3          0.72831200          ActNor.EstInrToBdy[2]

Q4          0.40593700          ActNor.EstInrToBdy[3]

GPS sec                1275838559         ActNor.EstTime

MPS Cmd Vector X          0.208432000

MPS Cmd Vector Y          0.901311000

MPS Cmd Vector Z          0.379731000

GPS sec                1275838559         ActNor.EstTime

UTC time             06/10/2020 15:35:45        output

CSS Angle TLM  0.958588             

CSS Sun-Pointing Angle 1.917176             

                                06 June 20 @22:00

CSS Angle TLM  0.744936             

CSS Sun-Pointing Angle 1.489872             

                                10 June 20 @15:00

Pre-Burn                            

Thruster 1           10544    06 June 20 @22:00

Thruster 2           10240   

Thruster 3           13216   

Thruster 4           13520   

Post-Burn                           

Thruster 1           10800    10 June 20 @15:00

Thruster 2           10496   

Thruster 3           13488   

Thruster 4           13792   

Number of Pulses                           

Thruster 1           256        

Thruster 2           256        

Thruster 3           272        

Thruster 4           272        

Thruster Pairs                   

Thruster 1 & 2    512        

Thruster 3 & 4    544        

 

 

 

 

Sheral Wesley  |  Principal Engineer, Satellite Systems

Northrop Grumman Corporation  |  Space Systems

O: 703-406-5641  |  C: 202-236-0802  |  sheral.wesley@ngc.com