Consider a satellite in orbit around a planet, as shown in the figure above. The (x, y) position of the satellite at time tis determined from the equations in the image above.

and T is the time in days it takes for the satellite to make one full revolution. Write a function that returns two column vectors: the x-position and y-position of the satellite at each day during one full revolution. The function should accept one input argument, a row vector M = [a b T].Any root find should meet the criteria aMATLAB functions other than basic math functions (trigonometric functions, sqrt, abs, etc.)

satellite x = a(cos E - e) y = a1 - 2 sin E planet 210 E=t+e sin E T b satellite x = a(cos E - e) y = a1 - 2 sin E planet 210 E=t+e sin E T b