All,

     The apogee contact was nominal. The sun maneuver was successful. During the contact I was able to uplink the Orbit #604 Version 2 ATS. The static Z rate was set to 4.160 and the FDC totals were reset.

 

Tasks Accomplished:

CAR # 1308 Orbit #604 version 2 ATS uplink

   IBEX_2023_099_o0604a_v002 91 Cmds

Reset FDC totals

Set Static Z rate 4.155 -> 4.160

 

Results from the Sun Maneuver:

CSS Angle TLM 0.9976

CSS Sun-Pointing Angle 1.9952

  01 Apr 23@16:00:00

CSS Angle TLM 0.939203

CSS Sun-Pointing Angle 1.878406

  05 Apr 23@13:00:00

Pre-Burn   

Thruster 1 2400 01 Apr 23@16:00:00

Thruster 2 2320

Thruster 3 2848

Thruster 4 2928

Post-Burn  

Thruster 1 2480 05 Apr 23@13:00:00

Thruster 2 2400

Thruster 3 3168

Thruster 4 3248

Number of Pulses  

Thruster 1 80

Thruster 2 80

Thruster 3 320

Thruster 4 320

Thruster Pairs  

Thruster 1 & 2 160

Thruster 3 & 4 640