All,

The apogee contact was nominal for command/telemetry and the sun maneuver successful

Results from the sun maneuver

Q1          0.64042700

Q2          -0.47794700

Q3          -0.09971680

Q4          0.59285500

GPS sec 1415221603

UTC time              11/09/2024 21:06:29

CSS Angle TLM   0.692386           

CSS Sun-Pointing Angle  1.384772           

                                03 Nov 24 @13:30:00

CSS Angle TLM   0.674056           

CSS Sun-Pointing Angle  1.348112           

                                09 Nov 24 @20:30:00

Pre-Burn                            

Thruster 1           8464     03 Nov 24 @13:30:00

Thruster 2           8256    

Thruster 3           10000  

Thruster 4           10208  

Post-Burn                           

Thruster 1           8800     09 Nov 24 @20:30:00

Thruster 2           8592    

Thruster 3           10592  

Thruster 4           10800  

Number of Pulses

Thruster 1           336       

Thruster 2           336       

Thruster 3           592       

Thruster 4           592       

Thruster Pairs

Thruster 1 & 2   672       

Thruster 3 & 4   1184    

Best Regards,

Sheral Wesley  | Sr Principal Engineer, Satellite Systems

Northrop Grumman Corporation  |  Space Systems

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