All,

   The apogee contact was nominal and the sun maneuver was successful. The star percent valid was at 21, so we were unable to set the static Z rate. The Orbit 590 ATS was successfully uplinked.

 

Tasks Accomplished:

CAR # 1279 Orbit #590 ATS uplink

    IBEX_2022_338_o0590a_v001 98 cmds

 

Results from the Sun Maneuver:

CSS Angle TLM 0.228957

CSS Sun-Pointing Angle 0.457914

  25 Nov 22@07:30:00

CSS Angle TLM 0.901789

CSS Sun-Pointing Angle 1.803578

  30 Nov 22@19:00:00

Pre-Burn   

Thruster 1 736 25 Nov 22@07:30:00

Thruster 2 736

Thruster 3 1040

Thruster 4 1040

Post-Burn  

Thruster 1 1120 30 Nov 22@19:00:00

Thruster 2 1072

Thruster 3 1616

Thruster 4 1664

Number of Pulses  

Thruster 1 384

Thruster 2 336

Thruster 3 576

Thruster 4 624

Thruster Pairs  

Thruster 1 & 2 720

Thruster 3 & 4 1200