Mean Motion of Satellite Formula

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Mean Motion is angular speed required for a body to complete an orbit, assuming constant speed in circular orbit that takes same time as variable speed elliptical orbit of actual body. Check FAQs
n=[GM.Earth]asemi3
n - Mean Motion?asemi - Semi Major Axis?[GM.Earth] - Earth’s Geocentric Gravitational Constant?

Mean Motion of Satellite Example

With values
With units
Only example

Here is how the Mean Motion of Satellite equation looks like with Values.

Here is how the Mean Motion of Satellite equation looks like with Units.

Here is how the Mean Motion of Satellite equation looks like.

0.045Edit=4E+14581.7Edit3
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Mean Motion of Satellite Solution

Follow our step by step solution on how to calculate Mean Motion of Satellite?

FIRST Step Consider the formula
n=[GM.Earth]asemi3
Next Step Substitute values of Variables
n=[GM.Earth]581.7km3
Next Step Substitute values of Constants
n=4E+14m³/s²581.7km3
Next Step Convert Units
n=4E+14m³/s²581700m3
Next Step Prepare to Evaluate
n=4E+145817003
Next Step Evaluate
n=0.0450008059755109rad/s
LAST Step Rounding Answer
n=0.045rad/s

Mean Motion of Satellite Formula Elements

Variables
Constants
Functions
Mean Motion
Mean Motion is angular speed required for a body to complete an orbit, assuming constant speed in circular orbit that takes same time as variable speed elliptical orbit of actual body.
Symbol: n
Measurement: Angular VelocityUnit: rad/s
Note: Value should be greater than 0.
Semi Major Axis
The Semi major axis can be used to determine the size of satellite's orbit. It is half of the major axis.
Symbol: asemi
Measurement: LengthUnit: km
Note: Value should be greater than 0.
Earth’s Geocentric Gravitational Constant
Earth’s Geocentric Gravitational Constant the gravitational parameter for the Earth as the central body.
Symbol: [GM.Earth]
Value: 3.986004418E+14 m³/s²
sqrt
A square root function is a function that takes a non-negative number as an input and returns the square root of the given input number.
Syntax: sqrt(Number)

Other formulas in Satellite Orbital Characteristics category

​Go Anomalistic Period
TAP=2πn
​Go Local Sidereal Time
LST=GST+Elong
​Go Mean Anomaly
M=E-esin(E)
​Go Nominal Mean Motion
no=[GM.Earth]asemi3

How to Evaluate Mean Motion of Satellite?

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.

FAQs on Mean Motion of Satellite

What is the formula to find Mean Motion of Satellite?
The formula of Mean Motion of Satellite is expressed as Mean Motion = sqrt([GM.Earth]/Semi Major Axis^3). Here is an example- 4.7E-6 = sqrt([GM.Earth]/581700^3).
How to calculate Mean Motion of Satellite?
With Semi Major Axis (asemi) we can find Mean Motion of Satellite using the formula - Mean Motion = sqrt([GM.Earth]/Semi Major Axis^3). This formula also uses Earth’s Geocentric Gravitational Constant and Square Root (sqrt) function(s).
Can the Mean Motion of Satellite be negative?
No, the Mean Motion of Satellite, measured in Angular Velocity cannot be negative.
Which unit is used to measure Mean Motion of Satellite?
Mean Motion of Satellite is usually measured using the Radian per Second[rad/s] for Angular Velocity. Radian per Day[rad/s], Radian per Hour[rad/s], Radian per Minute[rad/s] are the few other units in which Mean Motion of Satellite can be measured.
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