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Consider a satellite of mass m moving in a circular orbit around the Earth at a constant speed v and at an altitude h above t

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(a by bancing the force setallita S Mem (Reth)? muz Chetty V= s Me (Reth) required velocity (6) from the keplers law T 2 Чл.then velocity of sefaltice in orbit VE sme 8 6:6281012x5:97810²4 42000 x103 V = 0.978103 V = 970 ms required speed of setelliIf you have any doubt then mention in the commant.

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