Kepler's 3rd Law says that kR3 = T2 or, if we are solving for period where k is a constant based solely on the central body's mass:
(T2/T1) = (R2/R1)3/2
You can look up the T in days and R of orbit of the moon and solve tor the R of the satellite with a period of 1 day.
The velocity = 2πR/T (remember to convert units as needed)
Good luck!