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An artificial satellite circles around t...

An artificial satellite circles around the earth at a height of 2,200 km. Calculate its orbital velocity and period of revolution. Take,
Radius of earth `= 6.37 xx 10^(3) km`
Mass of earth `= 6 xx 10^(24) kg`
`G = 6.67 xx 10^(-11) Nm^(2) kg^(-2)`

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To solve the problem of calculating the orbital velocity and period of revolution of an artificial satellite at a height of 2,200 km above the Earth's surface, we can follow these steps: ### Step 1: Calculate the Radius of the Orbit The radius \( R \) of the satellite's orbit is the sum of the Earth's radius and the height of the satellite above the Earth's surface. Given: - Radius of the Earth \( R_E = 6.37 \times 10^3 \) km - Height of the satellite \( h = 2,200 \) km ...
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