Problem $2(30$ Points$)$ Our satellite is in geosynchronous orbit about the Earth $($radial distance of $42,164$ km$).$ When the satellite is in the direction directly away from the Sun, what is the magnitude of the delta$-$V required to reach Sun$-$Earth L$2,$ which is located $1\mathrm{.}501$x$106$ km away from the Earth? $=132\mathrm{.}71$x$109$ km$3/$s$2,=398,600$ km$3/$s$2,$ M$=1\mathrm{.}989$x$1030$ kg$,$ M$=5\mathrm{.}974$x$1024$ kg r$12=149\mathrm{.}60$x$106$ k