Match the Column I with Column II
For a satellite in circular orbit

(where `M_(E)` is the mass of the earth , m is the mass of the satellite and r is the radius of the orbit )

Options

A. A-r, B-s,C-q,D-p
B. A-q,B-p,C-r,D-s
C. A-p,B-q,C-s,D-r
D. A-s,B-r,C-p,D-q

Answer

D

Explanation

(d) Kinetic energy `=(GM_(E)m)/(2r),A-s`
Potential energy `=-(GM_(E)m)/( r),B-r`
Total energy `=-(GM_(E)m)/(2r),C-p`
Orbital velocity `=sqrt((GM_(E))/( r)),D-q`