All,

   The apogee contact was nominal. The inertial maneuver was successful. During the pass I reset the FDC Totals.

Tasks Accomplished:

Reset FDC Totals

Results from the Inertial Maneuver:

Q1 -0.07554540 ActNor.EstInrToBdy[0]

Q2 0.82830100 ActNor.EstInrToBdy[1]

Q3 -0.54469100 ActNor.EstInrToBdy[2]

Q4 0.10734300 ActNor.EstInrToBdy[3]

GPS sec 1356973290 ActNor.EstTime

UTC time 01/05/2023 17:01:16 output

MPS Diff 0.660 deg

MPS Cmd Vector X 0.266163000

MPS Cmd Vector Y -0.880742000

MPS Cmd Vector Z -0.391727000

CSS Angle TLM 0.589835

CSS Sun-Pointing Angle 1.17967

  31 Dec 22@09:30:00

CSS Angle TLM 1.29059

CSS Sun-Pointing Angle 2.58118

  05 Jan 23@09:30:00

Pre-Burn   

Thruster 1 2912 31 Dec 22@09:30:00

Thruster 2 2832

Thruster 3 4080

Thruster 4 4160

Post-Burn  

Thruster 1 3200 05 Jan 23@09:30:00

Thruster 2 3120

Thruster 3 4352

Thruster 4 4432

Number of Pulses  

Thruster 1 288

Thruster 2 288

Thruster 3 272

Thruster 4 272

Thruster Pairs  

Thruster 1 & 2 576

Thruster 3 & 4 544