All,

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

Q1 -0.39637800 ActNor.EstInrToBdy[0]

Q2 -0.58139100 ActNor.EstInrToBdy[1]

Q3 0.38459400 ActNor.EstInrToBdy[2]

Q4 0.59745900 ActNor.EstInrToBdy[3]

GPS sec 1221814906.000 ActNor.EstTime

MPS Cmd Vector X -0.999628000

MPS Cmd Vector Y 0.027259000

MPS Cmd Vector Z 0.000646000

MPS Diff 0.524

CSS Angle TLM 0.688418

CSS Sun-Pointing Angle 1.376836

  20 Sept 18 @ 0515

CSS Angle TLM 1.84737

CSS Sun-Pointing Angle 3.69474

  24 Sept 18 @ 09:00

Pre-Burn   

Thruster 1 5808 20 Sept 18 @ 0515

Thruster 2 5680

Thruster 3 6256

Thruster 4 6384

Post-Burn  

Thruster 1 6112 24 Sept 18 @ 09:00

Thruster 2 5952

Thruster 3 6560

Thruster 4 6720

Number of Pulses  

Thruster 1 304

Thruster 2 272

Thruster 3 304

Thruster 4 336

Thruster Pairs 

Thruster 1 & 2 576

Thruster 3 & 4 640

 

 

 

 

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

tim.perry@orbitalatk.com

Office (703) 406-5976

Cell (301) 606-1430

cid:image001.jpg@01D04F4E.6B1BECE0

 

 



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