calculate the speed of a satellite in an Orbit at a height of 1000 km from earth surface.
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Answered by
15
Orbital velocity of the satellite is -
vo = √[GM/(R+h)]
vo = √[6.67×10^-11 × 6×10^24 / (6.4×10^6 + 10^6)]
vo = √(4×10^14 / 7.4×10^6)
vo = √(54.054×10^6)
vo = 7.352×10^3 m
vo = 7.352 km
Hence, the speed of a satellite in an orbit is 7.352 km.
Hope this helps you...
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3
Explanation:
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