Find an equation for the elliptical orbit of the earth about the sun (at one focus) given an eccentricity of 0.017 and a major axis of 2.99 * 10^8 km.
The answer given is r = (1.49 * 10^8)/(1-0.017cos@)
I'm not sure how to use the value for the major axis, since r = ek/(1-ecos@). There's nothing ther about the major axis, only eccentricity and directrix.
The answer given is r = (1.49 * 10^8)/(1-0.017cos@)
I'm not sure how to use the value for the major axis, since r = ek/(1-ecos@). There's nothing ther about the major axis, only eccentricity and directrix.