All,

    The apogee contact was nominal, and the inertial maneuver was successful.

Results from the inertial maneuver:

Q1 -0.33223500 ActNor.EstInrToBdy[0]

Q2 0.56404100 ActNor.EstInrToBdy[1]

Q3 -0.14731800 ActNor.EstInrToBdy[2]

Q4 0.74146800 ActNor.EstInrToBdy[3]

GPS sec 1397055999 ActNor.EstTime

UTC time 04/13/2024 15:06:25 output

MPS Diff 0.691

MPS Cmd Vector X 0.93263000

MPS Cmd Vector Y 0.334848000

MPS Cmd Vector Z 0.134453000

CSS Angle TLM 0.413068

CSS Sun-Pointing Angle 0.826136

  08 Apr 24 @08:30:00

CSS Angle TLM 1.40889

CSS Sun-Pointing Angle 2.81778

  13 Apr 24 @15:00:00

Pre-Burn

Thruster 1 22496 08 Apr 24 @08:30:00

Thruster 2 21840

Thruster 3 30048

Thruster 4 30704

Post-Burn

Thruster 1 22768 13 Apr 24 @15:00:00

Thruster 2 22112

Thruster 3 30352

Thruster 4 31008

Number of Pulses

Thruster 1 272

Thruster 2 272

Thruster 3 304

Thruster 4 304

Thruster Pairs  

Thruster 1 & 2 544

Thruster 3 & 4 608

Kind regards,