All,

   The apogee contact was nominal for CMD and TLM. The inertial maneuver was successful.

Results from the Inertial Maneuver:

Q1 0.72325800 ActNor.EstInrToBdy[0]

Q2 0.12936800 ActNor.EstInrToBdy[1]

Q3 0.63363100 ActNor.EstInrToBdy[2]

Q4 0.24222700 ActNor.EstInrToBdy[3]

GPS sec 1362322923 ActNor.EstTime

UTC time 03/08/2023 15:01:49 output

MPS Diff 0.725 deg

MPS Cmd Vector X 0.980670000

MPS Cmd Vector Y -0.175691000

MPS Cmd Vector Z -0.086130000

CSS Angle TLM 0.990316

CSS Sun-Pointing Angle 1.980632

  04 Mar 23@06:30:00

CSS Angle TLM 1.13453

CSS Sun-Pointing Angle 2.26906

  08 Mar 23@15:00:00

Pre-Burn   

Thruster 1 752 04 Mar 23@06:30:00

Thruster 2 752

Thruster 3 928

Thruster 4 928

Post-Burn  

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

Thruster 2 1040

Thruster 3 1232

Thruster 4 1232

Number of Pulses  

Thruster 1 288

Thruster 2 288

Thruster 3 304

Thruster 4 304

Thruster Pairs  

Thruster 1 & 2 576

Thruster 3 & 4 608