Is there any position in the elliptical orbit of a satellite where the tangential component of the acceleration is greater than the component perpendicular to the tangential component? Is there any position in the elliptical orbit of a satellite where the tangential component of the acceleration is greater than the component perpendicular to the tangential component?
a.The existence of such a position depends on the parameters of the elliptical orbit.
b.No, such a position never exist in the elliptical orbit.
c.Yes, such a position always exist in the elliptical orbit.
