Physics > Gravitation > 6.0 Satellites

  Gravitation
    1.0 Newton's law of gravitation
    2.0 Variation of acceleration due to gravity
    3.0 Gravitational field
    4.0 Gravitational potential
    5.0 Gravitational potential energy
    6.0 Satellites
    7.0 Kepler's law of planetary motion
    8.0 Problem solving technique

6.1 Orbital speed of satellite

It is the minimum speed required to put the satellite into a given orbit around the earth.

For circular motion around the earth, necessary centripetal force to the satellite is being provided by the gravitational force exerted by the earth on the satellite.




So, $$\frac{{GMm}}{{{r^2}}} = \frac{{mv_0^2}}{r}$$ $${v_0} = \sqrt {\frac{{GM}}{r}} $$ or $${v_0} = R\sqrt {\frac{{GM}}{{{R^2}r}}} $$ As $\left( {\frac{{GM}}{{{R^2}}} = g} \right)$. So, $${v_0} = R\sqrt {\frac{g}{r}} $$ We can write, $${v_0} = R\sqrt {\frac{g}{{R + h}}} $$ or $${v_0} = \sqrt {\frac{g}{{\left( {\frac{1}{R} + \frac{h}{{{R^2}}}} \right)}}} $$ As $\left( {h < < R} \right)$. So, $${v_0} = \sqrt {gR} $$

1. So, the orbital speed of a satellite is independent of the mass of the satellite. The orbital speed of satellite depends upon the mass and radius of the earth/planet around which the revolution of the satellite is taking place.

2. The direction of orbital speed of a satellite at an instant is along the tangent to the orbital path of the satellite at that instant.

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