Orbital velocity is equal to √g/g+h how here it is √GMe/Re+h
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Radius of orbit (R): Distance between satellite and centre of earth
Orbital velocity of a satellite orbiting with radius R is
v = √(GM / R)
[Note: Here R is radius of orbit (not radius of Earth)]
If satellite is at height H from earth’s surface then
v = √[GM / (Re + H)]
Here Re is radius of Earth
Orbital velocity of a satellite orbiting with radius R is
v = √(GM / R)
[Note: Here R is radius of orbit (not radius of Earth)]
If satellite is at height H from earth’s surface then
v = √[GM / (Re + H)]
Here Re is radius of Earth
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