using Matlab

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 Fmg are: Fc=ms(T2r)2Fg=GrMEms 2023 Winter: BE 1500 - Quiz 1 (100 Points) Name: Milad Eeso c. (7 Points) Compute the vector (named FG) of gravitational force (Fmg) with the following parameters: The satellite mass ms is 4000kg, the mass of the Earth ME is 5.97361024kg, and the gravitational constant G is 6.674281011 d. (3 Points) Write a script with all calculations from the above three sections (a, b, and c) and you should have created three vectors r, FC, and FG in the script. e. (5 Points) Copy and paste the codes from the provided script (geoPlot.m) to the bottom of your script from step (d) and run the combined script. From observation on the plot, what is the r value of the intersection point? That r value is the GEO orbital radius