All,

 

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

 

Q1          -0.45593300        ActNor.EstInrToBdy[0]

Q2          -0.56338800        ActNor.EstInrToBdy[1]

Q3          0.49161700          ActNor.EstInrToBdy[2]

Q4          0.48273400          ActNor.EstInrToBdy[3]

GPS sec                1222678921.000 ActNor.EstTime

MPS Cmd Vector X          -0.991748000

MPS Cmd Vector Y          -0.113171000

MPS Cmd Vector Z          -0.060230000

MPS Diff              0.557

CSS Angle TLM  0.333965             

CSS Sun-Pointing Angle 0.66793

                                28 Sept 18 @ 12:30

CSS Angle TLM  0.958792             

CSS Sun-Pointing Angle 1.917584             

                                4  Oct 18 @ 09:00

Pre-Burn                            

Thruster 1           6384       28 Sept 18 @ 12:30

Thruster 2           6224      

Thruster 3           6848      

Thruster 4           7008      

Post-Burn                           

Thruster 1           6656       4  Oct 18 @ 09:00

Thruster 2           6496      

Thruster 3           7152      

Thruster 4           7312      

Number of Pulses                          

Thruster 1           272        

Thruster 2           272        

Thruster 3           304        

Thruster 4           304        

Thruster Pairs                   

Thruster 1 & 2    544        

Thruster 3 & 4    608        

 

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

OCO2 MOC#: (703) 429 - 7015

Mobile#: (240) 328 - 2098

Eric.Chubin@ngc.com
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