All,

The perigee passes were nominal for CMD and TLM. The Inertial maneuver was successful.

The following was accomplished:

Reset the Master timer

Reset FDC Totals

SSR Dump -> Dump New

CAR #1038 ATS Upload -> IBEX-2019_152_o0449_V001 91 Cmd’s

Maneuver Results:

Q1 0.26075000 ActNor.EstInrToBdy[0]

Q2 0.51155300 ActNor.EstInrToBdy[1]

Q3 0.81386400 ActNor.EstInrToBdy[2]

Q4 0.08915660 ActNor.EstInrToBdy[3]

MPS Cmd Vector X 0.512818000

MPS Cmd Vector Y 0.791241000

MPS Cmd Vector Z 0.333099000

GPS sec 124585284.000 ActNor.EstTime

MPS Diff 0.547 deg

CSS Angle TLM 0.3499986

CSS Sun-Pointing Angle 0.6999972

18 May 19 @ 12:00

CSS Angle TLM 0.331613

CSS Sun-Pointing Angle 0.663226

22 May 19 @ 18:30

Pre-Burn

Thruster 1 11312 18 May 19 @ 12:00

Thruster 2 11024

Thruster 3 13600

Thruster 4 13888

Post-Burn

Thruster 1 11584 22 May 19 @ 18:30

Thruster 2 11296

Thruster 3 13904

Thruster 4 14192

Number of Pulses

Thruster 1 272

Thruster 2 272

Thruster 3 304

Thruster 4 304

Thruster Pairs

Thruster 1 & 2 544

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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