All, 

   The apogee contact for Orbit# 574 was nominal. The Inertial maneuver was successful.

GPS sec 1341914402         ActNor.EstTime

UTC time             07/15/2022 09:59:48       output

MPS Diff               0.671     deg

Q1          -0.37022900        ActNor.EstInrToBdy[0]

Q2          -0.41983100        ActNor.EstInrToBdy[1]

Q3          -0.38330500        ActNor.EstInrToBdy[2]

Q4          0.73467600          ActNor.EstInrToBdy[3]

MPS Cmd Vector X           -0.340964000

MPS Cmd Vector Y           0.866431000

MPS Cmd Vector Z           0.364747000

CSS Angle TLM   0.361536             

CSS Sun-Pointing Angle 0.723072             

                                10 July 22 @18:00:00

CSS Angle TLM   0.326259             

CSS Sun-Pointing Angle 0.652518             

                                15 July 22 @10:00:00

Pre-Burn                            

Thruster 1            1984       10 July 22 @18:00:00

Thruster 2            1920      

Thruster 3            2464      

Thruster 4            2528      

Post-Burn                           

Thruster 1            2224       15 July 22 @10:00:00

Thruster 2            2160      

Thruster 3            2704      

Thruster 4            2768      

Number of Pulses                           

Thruster 1            240        

Thruster 2            240        

Thruster 3            240        

Thruster 4            240        

Thruster Pairs                   

Thruster 1 & 2    480        

Thruster 3 & 4    480        

Sheral Wesley  | Sr Principal Engineer, Satellite Systems

Northrop Grumman Corporation  |  Space Systems 

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