R= radius of moon
h= distance of satellite from moon's surface,
M = mass of moon,
G= Gravitational constant
Time period of a satellite = T = 2π(r)/v
let orbit radius = R + h =r
R = 1740 + 94 = 1844 km = 1.844 E6 m
M = mass of moon = 7.348E22 kg
T = 2π√[R³/(GM)]
= (2*(3.14)*((1740+94)*(10^3))^3/2)/ sqrt ((6.67*10^-11)*(7.34 × 10^22)) = 7032 sec = 1.9999337638883334 hr or approximately 2 hrs.