The diagrammatical representation for motion of jet is shown below:

The expression for the Mach number is given as:
\(\begin{aligned}{c}{\rm{Mach}}\;{\rm{number}} &= \frac{u}{c}\\\frac{c}{u} &= \frac{1}{{{\rm{Mach}}\;{\rm{number}}}}\end{aligned}\)
The angle of shock cone is calculated below:
\(\begin{aligned}{c}\theta &= {\sin ^{ - 1}}\left( {\frac{c}{u}} \right)\\ &= {\sin ^{ - 1}}\left( {\frac{1}{{{\rm{Mach number}}}}} \right)\\ &= {\sin ^{ - 1}}\left( {\frac{1}{{{\rm{2}}{\rm{.0}}}}} \right)\\ = 30^\circ \end{aligned}\)
The distance of jet relative to observer is calculated below:
\(\begin{aligned}{c}\tan \theta &= \frac{h}{d}\\d &= \frac{h}{{\tan \theta }}\\ &= \frac{{\left( {9500\;{\rm{m}}} \right)}}{{\tan \left( {30^\circ } \right)}}\\ &= 16454.5\;{\rm{m}}\end{aligned}\)
Hence, the plane is at a distance of \(16454.5\;{\rm{m}}\) at which the observer hears the sonic boom.