The amount of energy needed to increase the radius of orbit of a 500-kg satellite from its original orbit r-10 000 of radius 10 000 km can be modelled by the function E = 2: where E is the energy, in r Joules, and r is the new radius, in kilometers. a) Determine x-intercept(s) if it exists. b) Determine y-intercept(s) if it exists. c) Determine the equations of the horizontal asymptote if it exists. d) Determine the equations of the vertical asymptote(s) if it exists.

The amount of energy needed to increase the radius of orbit of a 500-kg satellite from its original orbit r-10 000 of radius 10 000 km can be modelled by the function E = 2: where E is the energy, in r Joules, and r is the new radius, in kilometers. a) Determine x-intercept(s) if it exists. b) Determine y-intercept(s) if it exists. c) Determine the equations of the horizontal asymptote if it exists. d) Determine the equations of the vertical asymptote(s) if it exists.