The orbital period of the satellite can be synchronized with mars' rotation, whose period is 24.6 hours. determine the required orbital radius for this to occur.

From formula we get redius^3 = (period^2 * (mass of Mars) * (Gravitational acceleration))) / 4*pi^2 From Into this equation put period = 8.86 * 10^4 sec, mass of mars = 6.39*10^23 kg, Gravitational acceleration = 6.67*10^-11 and pi = 22/7 and get value of r which is 2.7 * 10^7 meters