All,

   The perigee contacts were nominal. The inertial maneuver was successful. The Orbit 599 ats was uplinked and the spacecraft clock was set. The SSR was dumped and there were no errors in the dump.

Tasks Accomplished:

CAR # 1293 Orbit # 599 ATS upload

    IBEX_2023_054_o0599a_v001 103 commands

SSR Dump -> Dump New

Reset FDC Totals

Set the Spacecraft Clock

Reset the master Timer

Results from the Inertial Maneuver:

Q1 -0.30102800 ActNor.EstInrToBdy[0]

Q2 0.72148800 ActNor.EstInrToBdy[1]

Q3 -0.50744200 ActNor.EstInrToBdy[2]

Q4 0.36240900 ActNor.EstInrToBdy[3]

GPS sec 1360378844 ActNor.EstTime 

UTC time 02/14/2023 03:00:30 output

MPS Diff 0.631 deg

MPS Cmd Vector X 0.830284000

MPS Cmd Vector Y -0.507285000

MPS Cmd Vector Z -0.230848000

CSS Angle TLM 0.437902

CSS Sun-Pointing Angle 0.875804

  12 Feb 23@19:00:00

CSS Angle TLM 0.776069

CSS Sun-Pointing Angle 1.552138

  14 Feb 23@03:00:00

Pre-Burn

Thruster 1 832 12 Feb 23@19:00:00

Thruster 2 832

Thruster 3 1472

Thruster 4 1472

Post-Burn

Thruster 1 1168 14 Feb 23@03:00:00

Thruster 2 1168

Thruster 3 1840

Thruster 4 1840

Number of Pulses

Thruster 1 336

Thruster 2 336

Thruster 3 368

Thruster 4 368

Thruster Pairs 

Thruster 1 & 2 672

Thruster 3 & 4 736