All,

    During the apogee contact the flight computer reset @15:14:41. Prior to the reset the apogee inertial maneuver was successful. We do show the CEU 5 Volt is on and the payload has been safed. I have scheduled the following contact for later today: USHI02 02/18/23 049 18:00:00 - 19:30:00. This contact will be used to recover the spacecraft bus and the next available time will be on 21 Feb. We will recover the payload at that time. I will post the new time when they have been scheduled.

Results from the Inertial Maneuver:

Q1 0.46119300 ActNor.EstInrToBdy[0]

Q2 0.61936900 ActNor.EstInrToBdy[1]

Q3 0.10152500 ActNor.EstInrToBdy[2]

Q4 0.62719700 ActNor.EstInrToBdy[3]

GPS sec 1360767681 ActNor.EstTime

UTC time 02/18/2023 15:01:07 output

MPS Diff 0.727 deg

MPS Cmd Vector X 0.871664000

MPS Cmd Vector Y -0.445957000

MPS Cmd Vector Z -0.203283000

CSS Angle TLM 0.776069

CSS Sun-Pointing Angle 1.552138

  14 Feb 23@03:00:00

CSS Angle TLM 1.94269

CSS Sun-Pointing Angle 3.88538

  18 Feb 23@15:00:00

Pre-Burn   

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

Thruster 2 1168

Thruster 3 1840

Thruster 4 1840

Post-Burn  

Thruster 1 1488 18 Feb 23@15:00:00

Thruster 2 1440

Thruster 3 2160

Thruster 4 2208

Number of Pulses  

Thruster 1 320

Thruster 2 272

Thruster 3 320

Thruster 4 368

Thruster Pairs  

Thruster 1 & 2 592

Thruster 3 & 4 688