Consider adiabatic flow of air through a duct. At a given point in the duct, velocity of air is 300 m/s, temperature is 330 K and pressure is 180 kPa. Assume that the air behaves as a perfect gas with constant \(c_p = 1.005 \, \text{kJ/kg.K}\). The stagnation temperature at this point is \(\underline{\hspace{1cm}}\) K (round off to two decimal places).