can you calculate the orbital velocity of satelliteborbiting at an altitude of 500 km.Data: G=6.673 × 10 power of -11 SI units, M =5.972× 10 power of 24 kg ,R = 6371000 m, h= 500000 m.Solve with steps.
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sorry I am week in maths
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so because of this reason I do no the answer
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