Solution:
Solution
Orbital velocity $$=\sqrt { \dfrac { GM }{ r } } $$
Where $$r$$ is the distance of satellite from the centre of earth.
$$V=\sqrt { \dfrac { GM }{ 2R } } $$
$${ V }^{ 1 }=\sqrt { \dfrac { GM }{ 3R } \times \dfrac { 2 }{ 2 } } $$
$${ V }^{ 1 }=\sqrt { \dfrac { 2 }{ 3 } } \sqrt { \dfrac { GM }{ 2R } } $$
$${ V }^{ 1 }=\sqrt { \dfrac { 2 }{ 3 } } V$$