Tangential speed vT, for the satellite that orbits the earth from a distance 3R is : vT= v0/3.
Linear component of the speed along any point of the circle involved in the circular motion is called tangential speed.
Given;
Vo is Speed ; R is the distance of center of the earth
Fo is the force exerted on satellite
Let vT be tangential speed
For the satellite, gravitational force (Fg)is equal to centripetal force(Fc),
Hence, Fg = Fc = Fo
GMm/R² = mvo/3R²
Thus, GM = (v0)²R
As given, R = 3R
So, GMm/3R² = m(v0)²/3R
GMm/3R² = m(vT)²/3R
So, GM= 9R * (vT)²
Now, (v0)²R = 9(vT)²R
(vT)²= (v0)²/9
So, vT= v0/3
Therefore, the tangential speed, vT, for the satellite that orbits the earth from distance 3R is v0/3.
To know more about tangential speed, refer
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