Write a Matlab function to compute the time elapsed (t) since periapsis crossing, given; The mean orbit rate (n), The eccentricity (e), and the true anomaly (). Test your function with the following inputs:

(a) n = 0.001, e = 0.01, = /2 rad.

(b) n = 0.00001, e = 0.3, = rad.

also write a short script to run the above tests