All,

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

 

 

Q1 -0.53000800 ActNor.EstInrToBdy[0]

Q2 0.49246300 ActNor.EstInrToBdy[1]

Q3 -0.55383800 ActNor.EstInrToBdy[2]

Q4 0.41211100 ActNor.EstInrToBdy[3]

GPS sec 1236897374.000 ActNor.EstTime

MPS Cmd Vector X 0.993566000

MPS Cmd Vector Y -0.099644000

MPS Cmd Vector Z -0.053835000

MPS Diff 0.652 deg

CSS Angle TLM 1.03929

CSS Sun-Pointing Angle 2.07858

  10 Mar 19 @06:00

CSS Angle TLM 1.0178

CSS Sun-Pointing Angle 2.0356

  17 Mar 19 @22:30

Pre-Burn   

Thruster 1 7568 10 Mar 19 @06:00

Thruster 2 7392

Thruster 3 9008

Thruster 4 9184

Post-Burn  

Thruster 1 7744 17 Mar 19 @22:30

Thruster 2 7568

Thruster 3 9216

Thruster 4 9392

Number of Pulses  

Thruster 1 176

Thruster 2 176

Thruster 3 208

Thruster 4 208

Thruster Pairs  

Thruster 1 & 2 352

Thruster 3 & 4 416

 

 

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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