%matlab time series of flight through model
     clf
     load satradi009 -ascii;
     tim=satradi009 (:,1);
     den=satradi009 (:,2);
     %load OH2 -ascii;
%den2=OH2(:,5);
%semilogy(tim,den,'b-')
     plot(tim,den,'b-','linewidth',2)
    axis([-8000,8000,0,45])
     xlabel ('Time from CA (minutes)','fontsize',16)
     ylabel ('Distance (Saturn Radii)','fontsize',16)
     title('Trajectory Distances','fontsize',16)
%hold on
%plot(tim,den2,'r-o')
