All,

 

The perigee supports were nominal for CMD and TLM. The inertial maneuver was successful. Battery balancing was nominal.

The following was completed:

CAR #1039 Orbit #450 ATS, Uplinked 93 commands

Reset Master Timer

Dumped the SSR and set the pointers to 70000

               VC2 Count = 24615 with 11 sequence errors

 

 

Q1 -0.48966000 ActNor.EstInrToBdy[0]

Q2 -0.27621000 ActNor.EstInrToBdy[1]

Q3 -0.66384700 ActNor.EstInrToBdy[2]

Q4  0.49320200 ActNor.EstInrToBdy[3]

GPS sec 1243362568.000 ActNor.EstTime

MPS Diff 0.498 deg

MPS Cmd Vector X 0.377420000

MPS Cmd Vector Y 0.853224000

MPS Cmd Vector Z 0.359948000

CSS Angle TLM   0.26467

CSS Sun-Pointing Angle 0.52934  

27 May 19 @ 13:00

CSS Angle TLM 0.323851

CSS Sun-Pointing Angle 0.647702

31 May 19 @ 18:30

Pre-Burn                          

Thruster 1 11824  27 May 19 @ 13:00

Thruster 2 11536             

Thruster 3 14208             

Thruster 4 14496             

Post-Burn                         

Thruster 1 12128  31 May 19 @ 18:30

Thruster 2 11808             

Thruster 3 14496             

Thruster 4 14816             

Number of Pulses                          

Thruster 1 304   

Thruster 2 272   

Thruster 3 288   

Thruster 4 320   

Thruster Pairs                  

Thruster 1 & 2 576           

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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