All,

The apogee pass was nominal for CMD and TLM. The inertial maneuver was successful. Orbit 459 ATS (IBEX_2019_242_o0459a_v002) was uplinked during this pass.

Results from the Inertial maneuver:

Q1 0.08544890 ActNor.EstInrToBdy[0]

Q2 -0.62678800 ActNor.EstInrToBdy[1]

Q3 -0.45720100 ActNor.EstInrToBdy[2]

Q4 0.62514300 ActNor.EstInrToBdy[3]

GPS sec 1250764309 ActNor.EstTime

MPS Cmd Vector X -0.862471000

MPS Cmd Vector Y 0.468284000

MPS Cmd Vector Z 0.191974000

GPS sec 1250764309 ActNor.EstTime

UTC time 08/25/2019 10:31:35 output

MPS Diff 0.457 deg

CSS Angle TLM 0.467719

CSS Sun-Pointing Angle 0.935438

21 Aug 19 @ 11:30

CSS Angle TLM 0.360452

CSS Sun-Pointing Angle 0.720904

25 Aug 19 @ 10:30

Pre-Burn

Thruster 1 16752 21 Aug 19 @ 11:30

Thruster 2 16336

Thruster 3 19808

Thruster 4 20224

Post-Burn

Thruster 1 17056 25 Aug 19 @ 10:30

Thruster 2 16608

Thruster 3 20128

Thruster 4 20576

Number of Pulses

Thruster 1 304

Thruster 2 272

Thruster 3 320

Thruster 4 352

Thruster Pairs

Thruster 1 & 2 576

Thruster 3 & 4 672

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

tim.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430

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