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.

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16 May, 14:51

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Amaya Russell · Answer 1

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