%-------------------------------------------------------------------
%------------------------- Convert_Sat_State -----------------------
%-------------------------------------------------------------------
function [p, v] = Convert_Sat_State(pos, vel)
xkmper = 6378.135;
p = zeros(3,1);
v = zeros(3,1);
for i=1:3
p(i) = pos.v(i) * xkmper;
v(i) = vel.v(i) * xkmper / 60;
end