- Find the radius of the circular orbit of a satellite moving with an angular speed equal to the angular speed of earth's rotation.
- If the satellite is directly above the north pole at some instant, find the time it takes to come over the equatorial plane. Mass of the earth = 6 × 1024kg.
$\frac{2\pi}{\text{T}_{\text{e}}}=\frac{2\pi}{\text{T}_{\text{s}}}$ or $\frac{1}{24\times3600}=\frac{1}{2\pi\sqrt{\frac{(\text{R}+\text{h})^3}{\text{gR}^2}}}$
$3600=3.14\sqrt{\frac{(\text{R}+\text{h})^3}{\text{gR}^2}}$
$\frac{(\text{R}+\text{h})^2}{\text{gR}^2}=\frac{(12\times3600)^2}{(3.14)^2}$
$\frac{(6400+\text{h})^3\times10^9}{9.8\times(6400)^2\times10^6}=\frac{(12\times3600)^2}{(3.14)^2}$
$\frac{(6400+\text{h})^3\times10^9}{6272\times10^9}=432\times10^4$
$(6400+\text{h})^3=6272\times432\times10^4$
$6400+\text{h}=\big(6272\times432\times10^4\big)^{\frac{1}{3}}$
$\text{h}=\big(6272\times432\times10^4\big)^{\frac{1}{3}}-6400$
$=42300\text{cm}$
Time taken from north pole to equator $=\frac{1}{2}\text{t}$$=\Big(\frac{1}{2}\Big)\times6.28\sqrt{\frac{(43200+6400)^3}{10\times(6400)^2\times10^6}}$
$=3.14\sqrt{\frac{(497)^3\times10^6}{(64)^2\times10^{11}}}$
$=3.14\sqrt{\frac{497\times497\times497}{64\times64\times10^5}}$
$=6\text{ hour.}$






