Explain kepler's third law.
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According to keplers third law the square of time peruod of satelite around the sun is directly proportional to cube of its diatance from the sun of semi major axis.
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According to it the square of time period of revolution of planet around sun is directly proportional to the cube length of semi major axis.
i.e.
Here T is time period of revolution and R is the distance of planet from the earth.
When we remove the sign of directly proportional then we have have to write some constant.
So,
=
=
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