#### Answer

The radius of the orbit is $2.93\times 10^9~m$

#### Work Step by Step

We can convert the orbital period $T$ to units of seconds as:
$T = (1.0~day)(24~hr/day)(3600~s/hr)$
$T = 86,400~s$
We then use the orbital period and the mass of the sun $M_s$ to find the orbital radius $R$;
$T^2 = \frac{4\pi^2~R^3}{G~M_s}$
$R^3 = \frac{G~M_s~T^2}{4\pi^2}$
$R = (\frac{G~M_s~T^2}{4\pi^2})^{1/3}$
$R = (\frac{(6.67\times 10^{-11}~m^3/kg~s^2)(1.99\times 10^{30}~kg)(86,400~s)^2}{4\pi^2})^{1/3}$
$R = 2.93\times 10^9~m$
The radius of the orbit is $2.93\times 10^9~m$.