All,

The Perigee passes were nominal for CMD and TLM. The Inertial maneuver was successful and battery balancing was nominal.

The following was accomplished:

SSR Dump New and Set Pointer

Reset S/C Master Timer

CAR #1071 – ATS Upload – IBEX_2019_323_o0468a_v001 93 Commands

Results from the Inertial maneuver:

CSS Angle TLM   1.01046

CSS Sun-Pointing Angle   2.02092

 06 Nov 19 @ 23:30

CSS Angle TLM   0.855237            

CSS Sun-Pointing Angle   1.710474            

 10 Nov 19 @ 06:00

Pre-Burn            

Thruster 1 20240 06 Nov 19 @ 23:30

Thruster 2 19648             

Thruster 3 26272             

Thruster 4 26864             

Post-Burn

Thruster 1 20352 10 Nov 19 @ 06:00

Thruster 2 19728             

Thruster 3 26448             

Thruster 4 27072             

Number of Pulses

Thruster 1 112   

Thruster 2 80     

Thruster 3 176   

Thruster 4 208   

Thruster Pairs   

Thruster 1 & 2    192       

Thruster 3 & 4    384       

Eric Chubin
Mission Operations Engineer - OCO2, IBEX
Northrop Grumman Innovation Systems

OCO2 MOC#: (703) 429 - 7015

Mobile#: (240) 328 - 2098

Eric.Chubin@ngc.com