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+
+//Variable Declaration
+u=3.986*(10**14) //Earth's Gravitational constant(m^3/sec^2)
+
+//Calculation
+n=(2*3.14)/(24*60*60) //Mean Motion(rad/sec)
+a=((u/n**2)**(0.33333))/1000 //Radius of the orbit by kepler's 3rd law(km)
+
+//Result
+printf("The Radius of the circular orbit with 1 day period is : %d km",a)
+
+