<?xml version="1.0"?>
<initialize name="reset00" version="2.0">
  <!--
    This file sets up the spacecraft in a hig inclination elliptical orbit.
  -->

  <position frame="ECEF" unit="KM">
    <x> -2216.05436 </x>
    <y> -2837.09413 </y>
    <z> -6235.38291 </z>
  </position>

  <orientation unit="DEG" frame="LOCAL">
    <yaw>   90.0  </yaw>
  </orientation>

  <velocity unit="KM/SEC" frame="ECEF">
    <x>  6.938058 </x>
    <y> -5.419317 </y>
    <z>  0        </z>
  </velocity>

  <attitude_rate unit="DEG/SEC" frame="ECI">
    <y>  0.0 </y>
    <z>  0.0 </z>
  </attitude_rate>

</initialize>
