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Solve the following problem using Python, implementing the functions described below, one line at a time
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Description:
 def ecef2aer(x: float, y: float, z: float, lat0: float, lon0: float, h0: float, ell=None, deg: bool = True) -> Tuple[float, float, float]: """ gives azimuth, elevation and slant range from an Observer to a Point with ECEF coordinates. ECEF input location is with units of meters Parameters x : float or numpy.ndarray of float ECEF x coordinate (meters) y : float or numpy.ndarray of float ECEF y coordinate (meters) z : float or numpy.ndarray of float ECEF z coordinate (meters) lat0 : float Observer geodetic latitude lon0 : float Observer geodetic longitude h0 : float observer altitude above geodetic ellipsoid (meters) ell : Ellipsoid, optional reference ellipsoid deg : bool, optional degrees input/output (False: radians in/out) Returns ------- az : float or numpy.ndarray of float azimuth to target el : float or numpy.ndarray of float elevation to target srange : float or numpy.ndarray of float slant range [meters] """

    xEast, yNorth, zUp = ecef2enu(x, y, z, lat0, lon0, h0, ell, deg=deg)

    return enu2aer(xEast, yNorth, zUp, deg=deg)