using Matlab

using Matlab

using Matlab

using Matlab

using Matlab

4- (25 Points) Vector \& Script Question A geostationary orbit, also referred to as a geosynchronous equatorial orbit (GEO), is that an object in such an orbit has an orbital period equal to Earth's rotational period, one sidereal day, and so to ground observers it appears motionless, in a fixed position in the sky. To calculate the height of a geostationary orbit, for circular orbits around a body, the centripetal force (Fc) required to maintain the orbit is equal to the gravitational force (Fgg) acting on the satellite. Here Fc and Fch are: Fc=ms(T2r)2Fg=GrMEms a. (3 Points) Generate the radius vector r that starts from 30,000,000 meter and ends at 50,000,000 meter, with increment of 500,000 meter using colon operator. b. (7 Points) Compute the vector (named FC) of centripetal force (Fc) with the following parameters: The satellite mass ms is 4000kg, and orbital period T is 86164.09054 second (note: it is about 23.94 hours)