A) \[{{v}_{1}}={{v}_{2}}\]
B) \[{{v}_{1}}<{{v}_{2}}\]
C) \[{{v}_{1}}>{{v}_{2}}\]
D) \[\frac{{{v}_{1}}}{{{r}_{1}}}=\frac{{{v}_{2}}}{{{r}_{2}}}\]
Correct Answer: B
Solution :
\[v=\sqrt{\frac{GM}{r}}\]if \[{{r}_{1}}>{{r}_{2}}\] then \[{{v}_{1}}<{{v}_{2}}\] Orbital speed of satellite does not depends upon the mass of the satelliteYou need to login to perform this action.
You will be redirected in
3 sec