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A plenet moving along an elliptical orbit is closest to the su

Question

A plenet moving along an elliptical orbit is closest to the sun at a distance $r_{1}$ and farthest away at a distance of $r_{2}$ . If $v_{1}$ and $v_{2}$ are the linear velocities at these points respectively, then the ratio $\frac{v _{1}}{v _{2}}$ is

r_{2} / r_{1}

(r_{2} / r_{1})^{2}

r_{1} / r_{2}

(r_{1} / r_{2})^{2}

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Lucas Discussed

A plenet moving along an elliptical orbit is closest to the sun at a distance

r_{1}

and farthest away at a distance of

r_{2}

. If

v_{1}

and

v_{2}

are the linear velocities at these points respectively, then the ratio

\frac{v _{1}}{v _{2}}

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Question Text

A plenet moving along an elliptical orbit is closest to the sun at a distance

r_{1}

and farthest away at a distance of

r_{2}

. If

v_{1}

and

v_{2}

are the linear velocities at these points respectively, then the ratio

\frac{v _{1}}{v _{2}}

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