All,

    The perigee contacts were nominal. The inertial maneuver was successful. The orbit 601 ATS was uplinked. The SSR was downlinked and the star tracker image dump was completed.

Tasks Accomplished:

Procedure S924-OP31212 Star Tracker Image Dump

CAR #1299 orbit 601 ATS uplink

   IBEX_2023_072_o0601a_v001

Reset Master Timer

Reset FDC Totals

Results from the Inertial Maneuver:

Q1 -0.55634600 ActNor.EstInrToBdy[0]

Q2 0.46482400 ActNor.EstInrToBdy[1]

Q3 -0.57599600 ActNor.EstInrToBdy[2]

Q4 0.37768700 ActNor.EstInrToBdy[3]

GPS sec 1362727854 ActNor.EstTime

UTC time 03/13/2023 07:30:40 output

MPS Diff 0.604 deg

MPS Cmd Vector X 0.992667000

MPS Cmd Vector Y -0.106524000

MPS Cmd Vector Z -0.057146000

CSS Angle TLM 1.13453

CSS Sun-Pointing Angle 2.26906

  08 Mar 23@15:00:00

CSS Angle TLM 1.28314

CSS Sun-Pointing Angle 2.56628

  13 Mar 23@07:00:00

Pre-Burn   

Thruster 1 1040 08 Mar 23@15:00:00

Thruster 2 1040

Thruster 3 1232

Thruster 4 1232

Post-Burn  

Thruster 1 1392 13 Mar 23@07:00:00

Thruster 2 1312

Thruster 3 1520

Thruster 4 1600

Number of Pulses  

Thruster 1 352

Thruster 2 272

Thruster 3 288

Thruster 4 368

Thruster Pairs  

Thruster 1 & 2 624

Thruster 3 & 4 656