Question:
expression for orbital velocity moving around satellite
Answer:
V = √GmE/r
Where,
v = the orbital velocity of an object (m/s)
G = the universal gravitational constant, G = 6.673x10(-11) N∙m2/kg2
mE = the mass of the Earth (5.98 x 1024 kg)
r = the distance from the object to the center of the Earth
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