The original attitude monitoring software of the EUMETSAT Polar System Flight Dynamics Facility allowed the computation of mean attitude misalignment and AOCS sensor biases in a given processing time, assuming a nominal attitude law with constant misalignments. This system has been enhanced, computing the actual attitude evolution from the angular velocity reconstructed from the gyro data and estimating all the attitude and sensor parameters with a batch least square method based on the observations provided by the on- board optical sensors. The resultant attitude evolution can be propagated after a spectral analysis of the misalignment evolution through a Fast Fourier Transform. This software has been integrated in the Metop Flight Dynamics System and it is currently being used in routine operations to estimate the satellite short term attitude evolution (only one orbit of gyro data are daily available) providing a very useful information on the pointing stability of the platform.