A) \[-{{E}_{0}}\]
B) \[1.5{{E}_{0}}\]
C) \[2{{E}_{0}}\]
D) \[{{E}_{0}}\]
Correct Answer: C
Solution :
[c] \[P.E.=2T.E.\] \[\Rightarrow \]\[P.E.=2{{E}_{0}}\] In case of circular motion of satellite around the earth / planets revolving around sun/ electrons revolving in circular orbit P.E. = 2 T.E. and |K.E.|=|T.E.|].
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