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//Example 2.1.1
// Calculate the Orbital radius for a Geostationary Satellite
//Variable Declaration
T=86164.09 // Time Period for 1 sidereal day in Sec
//Calculation
u=(3.986004418*10^5)
a=((T^2*u)/(4*%pi^2))^(1/3)
//Result
printf("The Radius of the circular orbit with 1 day period is : %d km",a)
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