All,

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

Results from the Inertial maneuver:

Q1 0.67234300 ActNor.EstInrToBdy[0]

Q2 0.48289500 ActNor.EstInrToBdy[1]

Q3 -0.47271900 ActNor.EstInrToBdy[2]

Q4 0.30216500 ActNor.EstInrToBdy[3]                   

GPS sec 1259364781 ActNor.EstTime

UTC time 12/02/2019 23:32:47 output

MPS Diff 0.750 deg

CSS Angle TLM   0.561277            

CSS Sun-Pointing Angle   1.122554            

               28 Nov 19 @ 23:30

CSS Angle TLM   0.900921            

CSS Sun-Pointing Angle   1.801842            

               02 Dec 19 @ 23:30

Pre-Burn            

Thruster 1 21264 28 Nov 19 @ 01:30

Thruster 2 20592             

Thruster 3 27888             

Thruster 4 28560             

Post-Burn

Thruster 1 21680 02 Dec 19 @ 23:30

Thruster 2 21008             

Thruster 3 28320             

Thruster 4 28992             

Number of Pulses

Thruster 1 416   

Thruster 2 416   

Thruster 3 432   

Thruster 4 432   

Thruster Pairs   

Thruster 1 & 2    832       

Thruster 3 & 4    864       

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

OCO2 MOC#: (703) 429 - 7015

Mobile#: (240) 328 - 2098

Eric.Chubin@ngc.com