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//Variable Declaration
R=6371 //Mean Earth's radius(km)
e=0.0011501 //Eccentricity
a=7192.3 //Semimajor axis(km)
//Calculation
ra=a*(1+e) //Radius Vector at apogee(km)
rp=a*(1-e) //Radius Vector at perigee(km)
ha=ra-R //Apogee height(km)
hp=rp-R //Perigee height(km)
//Result
printf("The Apogee height for given orbital parameters is: %.2f km",ha)
printf("The Apogee height for given orbital parameters is: %.2f km",hp)
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