Could you answer it with python, please? I wanna all the steps will be included.

Exercise 3. Orbiting Satellite A geosynchronous satellite orbits above the same point on the Earth, find (a) the radius of its orbit (ans 4.22e+07 m) (b) the speed of its orbit (ans 3.02e+07 ms ) (c) the total mechanical energy associated with its orbit (ans -4.71e+08 J) The mass of the Earth is 5.97 x1024 kg. Newtons Universal gravitation constant G is given in the Scipy constants library as spc. G and the number of seconds in one day is given by spc.day where spc is the name used to identify the Scipy constants library. This is given in the file PH185Lab04cu.py Talonary 64 65 66 67 58 59 * Exercise 3 Tis the time in second for one day # G is Newton's Gravitation constant N is the mass of eth Earth in kG ET = spc.day *6 = spc.G S = 5.97e24 72 3 a) the radius of its orbit fimport scipy as spc r = (spc.GT+2)/(4*p1# 2) 5 b) the speed of its orbit 10.sqrt(07 c) the total mechanical energy associated with its, orbit