According to Kepler's first law, a comet should have an elliptic, parabolic, or hyperbolic orbit (with gravitational attractions from the planets ignored). In suitable polar coordinates, the position (r, 9) of a comet satisfies an equation of the form r = ß + e(r.cos 9), where ß is a constant and e is the eccentricity of the orbit, with 0≤e<1 for an ellipse, e = 1 for a parabola, and e> 1 for a hyperbola. Suppose observations of a newly discovered comet provide the data below. Determine the type of orbit, and predict where the comet will be when 9 = 4.4 (radians). 9 r 0.87 1.08 1.45 1.77 2.12 3.56 3.03 1.97 1.03 0.65 The comet has orbit. When 9 = 4.4 (radians), the comet will be at r = (Round to two decimal places as needed.)