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Q. The eccentricity of earths orbit is $0.0167$. The ratio of its maximum speed in its orbit to its minimum speed is:

ManipalManipal 2006Gravitation

Solution:

Eccentricity, $e=\frac{r_{\max }-r_{\min }}{r_{\max }+r_{\min }}=0.0167$
Therefore, $\frac{r_{\max }}{r_{\min }}=\frac{1+e}{1-e}$
$=\frac{1-0.0167}{1+0.0167}$
As angular momentum remains constant, hence
$r_{\max } \times v_{\min } =r_{\min } \times v_{\max }$
$\therefore \frac{v_{\max }}{v_{\min }}=\frac{r_{\max }}{r_{\min }} =\frac{1+0.0167}{1-0.0167}$
$=1.0339$