To solve this problem it is necessary to apply the concepts related to the orbital velocity of a satellite on earth.
This concept is expressed in the equation,
[tex]v = \sqrt{\frac{Gm_E}{r}}[/tex]
Where,
G = Universal Gravitational constant
[tex]m_E =[/tex] Mass of the Earth
Therefore the ratio of the velocity from two satellites is,
[tex]\frac{v_1}{v_2} = \sqrt{\frac{r_2}{r_1}}[/tex]
The ratio between the two satellites is the same, then
[tex]\frac{v_1}{v_2} = \sqrt{\frac{r}{r}}[/tex]
[tex]\frac{v_1}{v_2} = 1[/tex]
[tex]v_1 =v_2[/tex]
Therefore the correct option is B.