All,

The perigee contacts were nominal for CMD and TLM. The Inertial maneuver was successful and battery balancing was nominal.

The following was completed:

               SSR Dump

               Reset Master Timer

               CAR #1015 ATS Upload – IBEX_2019_014_o0434a_v001.scr

               Reset FDC Totals

Results from the Inertial Maneuver:

Q1 0.78278100 ActNor.EstInrToBdy[0]

Q2 0.27884100 ActNor.EstInrToBdy[1]

Q3 -0.03303950 ActNor.EstInrToBdy[2]

Q4 0.55534700 ActNor.EstInrToBdy[3]

GPS sec 1230724725.000 ActNor.EstTime

MPS Cmd Vector X 0.265226000

MPS Cmd Vector Y -0.880525000

MPS Cmd Vector Z -0.392851000

MPS Diff 0.898 deg

CSS Angle TLM   1.13522

CSS Sun-Pointing Angle   2.27044

                              01 Jan 18 @20:00

CSS Angle TLM   0.85638

CSS Sun-Pointing Angle   1.71276

                              05 Jan 18 @12:00

Pre-Burn

Thruster 1 3408 01 Jan 18 @20:00

Thruster 2 3312

Thruster 3 3984

Thruster 4 4080

Post-Burn

Thruster 1 3776 05 Jan 18 @12:00

Thruster 2 3680

Thruster 3 4384

Thruster 4 4480

Number of Pulses

Thruster 1 368

Thruster 2 368

Thruster 3 400

Thruster 4 400

Thruster Pairs

Thruster 1 & 2    736

Thruster 3 & 4    800

Eric Chubin
Mission Operations Engineer - OCO2, IBEX
Northrop Grumman Innovation Systems

OCO2 MOC#: (703) 429 - 7015

Mobile#: (240) 328 - 2098

Eric.Chubin@ngc.com

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