Question

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.

Answer 1

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