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//Example 2.1.3
//Elliptical Orbit
//Variable Declaration
re=6378.14
hp=1000
ha=4000
u=3.98600*((10)^5)
//Calculation
a=(2*re+hp+ha)/2
T=sqrt((4*(%pi^2)*(a^3)/u))
e=1-((re+hp)/a) //Eccentricity of orbit
//Result
printf("The period of orbit is : %f seconds",T)
disp(e,'Eccentricity of orbit')
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