All,

The Perigee contacts were nominal for command and telemetry. The sun maneuver was successful.

Tasks Accomplished:

On both perigee contacts - SSR Dump à Dump New

Dump back-orbit buffer

CAR #1276 Orbit 588 ATS Upload

                IBEX_2022_320_o0588a_v001.scr 88 cmds

Reset Master 18 day Timer

Set Spacecraft Clock

Reset AC/FDC failed totals

Results from the Sun Maneuver

CSS Angle TLM   1.96394                

CSS Sun-Pointing Angle 3.92788                

                                05 Nov 22@03:30:00

CSS Angle TLM   1.3106  

CSS Sun-Pointing Angle 2.6212  

                                07 Nov 22@11:00:00

Pre-Burn

Thruster 1            8400       05 Nov 22@03:30:00

Thruster 2            8160      

Thruster 3            10864   

Thruster 4            11104   

Post-Burn

Thruster 1            8576       07 Nov 22@11:00:00

Thruster 2            8288      

Thruster 3            11280   

Thruster 4            11568   

Number of Pulses

Thruster 1            176        

Thruster 2            128        

Thruster 3            416        

Thruster 4            464        

Thruster Pairs   

Thruster 1 & 2    304        

Thruster 3 & 4    880        

Eric Chubin  | Principal Engineer Satellite Systems

Northrop Grumman Corporation  |  Space Systems

O: 703-429-7015  |  C: 240-328-2098  |  eric.chubin@ngc.com