All,

  The perigee contacts were nominal and the inertial maneuver was successful. We upload the Hi background sweep table on the first contact. The Orbit 603 ATS was uplinked and the SSR was successfully dumped.

 

Tasks Accomplished:

CAR # 1269 2023 ISN Season & Hi Background test sweep table uplink procedure

  Pass #5 Upload Hi Background sweep table

CAR # 1303 Orbit #603 ATS uplink

   IBEX_20923_090_o0603a_v001 98 Cmds

SSR Dump -> Dump New

Reset Master Timer

 

Results from the Inertial Maneuver

Q1 0.66959300 ActNor.EstInrToBdy[0]

Q2 0.22868500 ActNor.EstInrToBdy[1]

Q3 0.66755900 ActNor.EstInrToBdy[2]

Q4 0.23176400 ActNor.EstInrToBdy[3]

     

GPS sec 1363514453 ActNor.EstTime

UTC time 03/22/2023 10:00:39 output

 

MPS Diff 0.851 deg

 

MPS Cmd Vector X 0.999941000

MPS Cmd Vector Y 0.009023000

MPS Cmd Vector Z -0.006126000

 

CSS Angle TLM 0.936282

CSS Sun-Pointing Angle 1.872564

  17 Mar 23@15:00:00

 

CSS Angle TLM 0.836031

CSS Sun-Pointing Angle 1.672062

  22 Mar 23@10:00:00

 

Pre-Burn   

Thruster 1 1664 17 Mar 23@15:00:00

Thruster 2 1584

Thruster 3 1840

Thruster 4 1920

Post-Burn  

Thruster 1 1842 22 Mar 23@10:00:00

Thruster 2 1744

Thruster 3 2000

Thruster 4 2080

Number of Pulses  

Thruster 1 178

Thruster 2 160

Thruster 3 160

Thruster 4 160

Thruster Pairs  

Thruster 1 & 2 338

Thruster 3 & 4 320