I am using GMAT to propagate satellite motion with Jacchia-Roberts atmosphere model. Here is a formula used from this model which is then used to estimate the variation in drag on a spacecraft due to heating by solar activity:
$$T_c(K) = 379 + 3.24\cdot F_{10.7} + 1.3[F_{10.7} – \overline{F}_{10.7}]$$
in which $F_{10.7}$ and $\overline{F}_{10.7}$(the average daily solar flux at a 10.7 cm wavelength for the day of interest and 81-day running average of $F_{10.7}$ centered on the day of interest, respectively) are used.
I would like to ask; where does GMAT take this coefficients from and where can I find the $\overline{F}_{10.7}$ in order i would like to implement Jacchia-Roberts?
As it is seen from definition, a values not only before but also after this day will be needed to calculate $\overline{F}_{10.7}$ but I couldn't find a resource in the internet providing me such information.