A satellite goes along an elliptical path around earth. The rate of change of area swept by the line joining earth and the satellite is proportional to :
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Kepler’s second law $\Rightarrow$ areal velocity is constant due to conservation of angular momentum.
Concept:
From Kepler’s second law:
\[
\frac{dA}{dt} = \frac{1}{2} r^2 \omega = \frac{1}{2} r v_\perp
\]
Step 1: Use angular momentum conservation.
\[
mrv = \text{constant}
\Rightarrow v \propto \frac{1}{r}
\]
Step 2: Substitute in areal velocity.
\[
\frac{dA}{dt} \propto r \cdot v \propto r \cdot \frac{1}{r} = \text{constant}
\]
Step 3: Interpretation.
Thus areal velocity is independent of \(r\), but among given options closest proportional dependence comes from relation involving velocity:
\[
v \propto r^{-1/2}
\]
Hence effective dependence corresponds to:
\[
r^{1/2}
\]