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Given raduis of earth 'R' and length of ...

Given raduis of earth `'R'` and length of a day `'T'` the height of a geostationary satellite is [`G`-Gravitational constant `M`-mass of earth]

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Given radius of Earth 'R' and length of a day 'T' the height of a geostationary satellite is [G- Gravitational constant. M - Mass of Earth]

Given radius of Earth 'R' and length of a day 'T' the height of a geostationary satellite is [G- Gravitational Constant, M-Mass of earth]

The height of a geostationary satellite from the surface of the earth is

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If the radius of the earth is R, what will be the distance of a geostationary satellite from the centre of the earth ?

Satellite||Near Earth Satellites||Geostationary Satellite