Nominal Mean Motion evaluator uses Nominal Mean Motion = sqrt([GM.Earth]/Semi Major Axis^3) to evaluate the Nominal Mean Motion, The Nominal Mean Motion 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. Nominal Mean Motion is denoted by no symbol.
How to evaluate Nominal Mean Motion using this online evaluator? To use this online evaluator for Nominal Mean Motion, enter Semi Major Axis (asemi) and hit the calculate button.