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Numericals · Q39

Q.Two satellites A and B are revolving around a planet. Their periods of revolution are 1 hour and 8 hours respectively. The radius of orbit of satellite B is 4×1044\times10^4 km. Find the radius of orbit of satellite A.

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By Kepler's third law (law of periods, also derivable for satellites from T2=4π2r3/GMT^2=4\pi^2r^3/GM), T2∝r3T^2\propto r^3 for satellites orbiting the same planet, so (TATB)2=(rArB)3.\left(\dfrac{T_A}{T_B}\right)^2=\left(\dfrac{r_A}{r_B}\right)^3. Given TA=1T_A=1 hour and TB=8T_B=8 hours: $$\left(\dfrac{1}{8}\right)^2=\dfrac{1}{64}=\left(\dfrac{r_A}{r_B}\right)^3\quad\Longrightarrow\quad\dfrac{r_A}{r_B}=\left(\dfrac{1}{64}\right)^ …

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