Question

vii) Calculate the speed of a satellite in an
orbit at a height of 1000 km from the
Earth's surface. M=5.98x10^24 kg, R =
6.4x10^6 m.
[Ans: 7.34 x10^3 m/s]​

Answer 1

Answer:

Answer:Explanation:formula of finding so=$\sqrt{Mce/t} =2\pi r/t \lim_{n \to \infty} a_n$in ... orbit at a height of 1000 km from the. Earth's surface. M=5.98x10^24 kg, R = 6.4