All,

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

   

Q1 -0.50054500 ActNor.EstInrToBdy[0]

Q2 0.26842500 ActNor.EstInrToBdy[1]

Q3 -0.00341254 ActNor.EstInrToBdy[2]

Q4 0.82303800 ActNor.EstInrToBdy[3]

GPS sec 1242997165.000 ActNor.EstTime

MPS Diff 0.520 deg

MPS Cmd Vector X 0.447381000

MPS Cmd Vector Y 0.824557000

MPS Cmd Vector Z 0.346346000

CSS Angle TLM 0.331613

CSS Sun-Pointing Angle 0.663226

  22 May 19 @ 18:30

CSS Angle TLM 0.26467

CSS Sun-Pointing Angle 0.52934

  27 May 19 @ 13:00

Pre-Burn   

Thruster 1 11584 22 May 19 @ 18:30

Thruster 2 11296

Thruster 3 13904

Thruster 4 14192

Post-Burn  

Thruster 1 11824 27 May 19 @ 13:00

Thruster 2 11536

Thruster 3 14208

Thruster 4 14496

Number of Pulses  

Thruster 1 240

Thruster 2 240

Thruster 3 304

Thruster 4 304

Thruster Pairs 

Thruster 1 & 2 480

Thruster 3 & 4 608

 

 

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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