Nominal Mean Motion Formula

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Nominal Mean Motion refers to the average rate at which a satellite orbits around a celestial body, such as the Earth. Check FAQs
no=[GM.Earth]asemi3
no - Nominal Mean Motion?asemi - Semi Major Axis?[GM.Earth] - Earth’s Geocentric Gravitational Constant?

Nominal Mean Motion Example

With values
With units
Only example

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

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

Here is how the Nominal Mean Motion equation looks like.

0.045Edit=4E+14581.7Edit3
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Nominal Mean Motion Solution

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

FIRST Step Consider the formula
no=[GM.Earth]asemi3
Next Step Substitute values of Variables
no=[GM.Earth]581.7km3
Next Step Substitute values of Constants
no=4E+14m³/s²581.7km3
Next Step Convert Units
no=4E+14m³/s²581700m3
Next Step Prepare to Evaluate
no=4E+145817003
Next Step Evaluate
no=0.0450008059755109rad/s
LAST Step Rounding Answer
no=0.045rad/s

Nominal Mean Motion Formula Elements

Variables
Constants
Functions
Nominal Mean Motion
Nominal Mean Motion refers to the average rate at which a satellite orbits around a celestial body, such as the Earth.
Symbol: no
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 Mean Motion of Satellite
n=[GM.Earth]asemi3

How to Evaluate Nominal Mean Motion?

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.

FAQs on Nominal Mean Motion

What is the formula to find Nominal Mean Motion?
The formula of Nominal Mean Motion is expressed as Nominal Mean Motion = sqrt([GM.Earth]/Semi Major Axis^3). Here is an example- 4.7E-6 = sqrt([GM.Earth]/581700^3).
How to calculate Nominal Mean Motion?
With Semi Major Axis (asemi) we can find Nominal Mean Motion using the formula - Nominal 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 Nominal Mean Motion be negative?
No, the Nominal Mean Motion, measured in Angular Velocity cannot be negative.
Which unit is used to measure Nominal Mean Motion?
Nominal Mean Motion 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 Nominal Mean Motion can be measured.
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