Given: $,G=6\mathrm{.}67{10}^{-11}N*\frac{m^2}{k}{g}^2$;$M_{\text{S}\text{u}\text{n}}=2\mathrm{.}00{10}^{30}kg$;$M_{\text{E}\text{a}\text{r}\text{t}\text{h}}=5\mathrm{.}97{10}^{24}kg$

Average distance of Earth from Sun $=1\mathrm{.}50{10}^{8}km$

The Solar and Heliospheric Observatory $($SOHO$)$ is a $1,850-$kg satellite in orbit at the L$1$ Lagrange point, located $1\mathrm{.}50{10}^{6}km$ from Earth and directly between Earth and the Sun. What are the magnitude and direction of the net gravitational force on this satellite?