A satellite of mass m revolves around earth or radius r at a height x from its surface if g is the accelaration due to gravity on the surface of the earth than the orbital speed of the satellite is
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mv²/(R+x) = GmM / (R+x)² and g = GM /R²
mv²/( R+x ) = m (GM/R²) R²/( R + x )²
v² = gR2/R+x
:. v = (gR² / R+x )^1/2
hope it helped!
mv²/( R+x ) = m (GM/R²) R²/( R + x )²
v² = gR2/R+x
:. v = (gR² / R+x )^1/2
hope it helped!
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