All,

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

Q1 -0.42869900 ActNor.EstInrToBdy[0]

Q2 -0.35058700 ActNor.EstInrToBdy[1]

Q3 -0.35892200 ActNor.EstInrToBdy[2]

Q4 0.75131900 ActNor.EstInrToBdy[3]

GPS sec 1151930000.000 ActNor.EstTime

MPS Cmd Vector X -0.226264000

MPS Cmd Vector Y 0.897743000

MPS Cmd Vector Z 0.377970000

MPS Diff 0.655

03 June 16 @0200

CSS Angle TLM 2.28662

CSS Sun-Pointing Angle 4.57324

07 June 16 @1200

CSS Angle TLM 1.9262

CSS Sun-Pointing Angle 3.8524

Pre-Burn 03 June 16 @0200

Thruster 1 14288

Thruster 2 13824

Thruster 3 18432

Thruster 4 18896

Post-Burn 07 June 16 @1200

Thruster 1 14544

Thruster 2 14080

Thruster 3 18720

Thruster 4 19184

Number of Pulses

Thruster 1 256

Thruster 2 256

Thruster 3 288

Thruster 4 288

Thruster Pairs

Thruster 1 & 2 512

Thruster 3 & 4 576

Timothy E.Perry

CRS, IBEX & OCO-2

Mission Operations

tim.perry@orbitalatk.com

Office (703) 406-5976

Cell (301) 606-1430

Corp Cell (571)-447-8977

cid:image001.jpg@01D04F4E.6B1BECE0

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