All,

The Apogee pass was nominal for CMD and TLM. The Inertial Maneuver was successful.

Results from the Inertial Maneuver:

CSS Angle TLM   0.863208            

CSS Sun-Pointing Angle   1.726416            

  22 Oct 19 @ 23:05

CSS Angle TLM   0.296075            

CSS Sun-Pointing Angle   0.59215

  27 Oct 19 @ 23:00

Pre-Burn

Thruster 1 19520 22 Oct 19 @ 23:05

Thruster 2 18928             

Thruster 3 25136             

Thruster 4 25728             

Post-Burn

Thruster 1 19664 27 Oct 19 @ 23:00

Thruster 2 19072             

Thruster 3 25328             

Thruster 4 25920             

Number of Pulses

Thruster 1 144   

Thruster 2 144   

Thruster 3 192   

Thruster 4 192   

Thruster Pairs   

Thruster 1 & 2    288       

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