Mean Motion of Satellite evaluator uses Mean Motion = sqrt([GM.Earth]/Semi Major Axis^3) to evaluate the Mean Motion, The Mean Motion of Satellite formula is defined as the angular speed required for a body to complete one orbit, assuming constant speed in a circular orbit which completes in the same time as the variable speed, elliptical orbit of the actual body. Mean Motion is denoted by n symbol.
How to evaluate Mean Motion of Satellite using this online evaluator? To use this online evaluator for Mean Motion of Satellite, enter Semi Major Axis (asemi) and hit the calculate button.