A satellite orbiting the Earth at 400 km above the surface of the Earth has a 2 m long antenna oriented perpendicular to the Earth's surface. At the equator the Earth's magnetic field is 8×10−5 T and is horizontal. Assuming the orbit to the circular, find emf induced across the ends of the antenna.(Given radius of earth Re =6400 Km)
"v=\\sqrt{\\frac{gR^2}{R+h}}=7.7~\\frac{km}s,"
"\\varepsilon=Blv=1.23~V."
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