The application discloses a
satellite orbit prediction method,
system, device and medium based on a gravity field vectorization calculation model, and the method comprises the following steps: establishing a motion equation of a
satellite in an inertial
system; constructing a gravity field fast calculation model; dividing a gradient formula of a gravity field potential position into a sum of a
harmonic part and a non-
harmonic part, and performing vectorization reconstruction to obtain a gravity field vectorization calculation model; obtaining a position and a
velocity vector of the
satellite at an initial moment, inputting the position and the
velocity vector into the motion equation of the satellite in the inertial
system, combining the gravity field vectorization calculation model, and solving the
satellite orbit by using a numerical integration method. The gravity field vectorization calculation model is numerically equivalent to a traditional loop
algorithm, the accuracy of the gravity field model is ensured without loss, the traditional
double loop structure is replaced by matrix operation, the calculation efficiency of a high-order gravity field is significantly improved, and therefore, the
satellite orbit prediction calculation efficiency is improved on the basis of ensuring the accuracy.