The period of a satellite,in a circular orbit near an equatorial plane,will not depend on

  • A
    The mass of the planet
  • B
    The radius of the planet
  • C
    The mass of the satellite
  • D
    All the above parameters

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If a satellite has to orbit the earth in a circular path every $6 \text{ hrs}$, at what distance from the surface of the earth should the satellite be placed (in $\text{ km}$)? (Radius of earth $R_e = 6400 \text{ km}$)
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$A$ planet revolves around the Sun in an elliptical orbit. When it is closest to the Sun,its distance from the Sun is $d_1$ and its velocity is $v_1$. When it is farthest from the Sun,its distance from the Sun is $d_2$. What is its velocity at that point?

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