An artificial satellite moving in a circular orbit at a distance $h$ from the centre of the earth has a total energy $E_{0}$ . Its potential energy is

- E_{0}

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1.5 E_{0}

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E_{0}

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2 E_{0}

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\frac{E_{0}}{2}

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Solution

The correct option is D $2 E_{0}$
Potential energy $= 2 \times$ total energy $= 2 E_{0}$

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