Circular Orbital Radius Given Velocity of Circular Orbit Solution

STEP 0: Pre-Calculation Summary
Formula Used
Orbit Radius = [GM.Earth]/Velocity of Circular Orbit^2
r = [GM.Earth]/vcir^2
This formula uses 1 Constants, 2 Variables
Constants Used
[GM.Earth] - Earth’s Geocentric Gravitational Constant Value Taken As 3.986004418E+14
Variables Used
Orbit Radius - (Measured in Meter) - The Orbit Radius is defined as the distance from the center of the orbit to the orbit's path.
Velocity of Circular Orbit - (Measured in Meter per Second) - Velocity of Circular Orbit is the speed of a body in a circular orbit.
STEP 1: Convert Input(s) to Base Unit
Velocity of Circular Orbit: 6.05 Kilometer per Second --> 6050 Meter per Second (Check conversion ​here)
STEP 2: Evaluate Formula
Substituting Input Values in Formula
r = [GM.Earth]/vcir^2 --> [GM.Earth]/6050^2
Evaluating ... ...
r = 10889978.6025545
STEP 3: Convert Result to Output's Unit
10889978.6025545 Meter -->10889.9786025545 Kilometer (Check conversion ​here)
FINAL ANSWER
10889.9786025545 10889.98 Kilometer <-- Orbit Radius
(Calculation completed in 00.020 seconds)

Credits

Creator Image
Hindustan Institute of Technology and Science (HITS), Chennai, Indian
Karavadiya Divykumar Rasikbhai has created this Calculator and 10+ more calculators!
Verifier Image
Verified by Anshika Arya
National Institute Of Technology (NIT), Hamirpur
Anshika Arya has verified this Calculator and 2500+ more calculators!

Circular Orbit Parameters Calculators

Orbital Period
​ LaTeX ​ Go Time Period of Orbit = 2*pi*sqrt((Orbit Radius^3)/([G.]*Central Body Mass))
Velocity of Circular Orbit
​ LaTeX ​ Go Velocity of Circular Orbit = sqrt([GM.Earth]/Orbit Radius)
Circular Orbital Radius
​ LaTeX ​ Go Orbit Radius = Angular Momentum of Circular Orbit^2/[GM.Earth]
Circular Orbital Radius Given Velocity of Circular Orbit
​ LaTeX ​ Go Orbit Radius = [GM.Earth]/Velocity of Circular Orbit^2

Circular Orbital Radius Given Velocity of Circular Orbit Formula

​LaTeX ​Go
Orbit Radius = [GM.Earth]/Velocity of Circular Orbit^2
r = [GM.Earth]/vcir^2

What is velocity of circular orbit ?

The velocity of a circular orbit, often referred to as orbital velocity, is the constant speed at which an object must travel to maintain a stable circular orbit around another body. It's the speed at which the gravitational force pulling the object towards the central body is balanced by the centrifugal force, which tends to make the object move in a straight line.

How to Calculate Circular Orbital Radius Given Velocity of Circular Orbit?

Circular Orbital Radius Given Velocity of Circular Orbit calculator uses Orbit Radius = [GM.Earth]/Velocity of Circular Orbit^2 to calculate the Orbit Radius, Circular Orbital Radius Given Velocity of Circular Orbit formula is defined as the distance from the center of the Earth to an object in circular orbit, which is a critical parameter in understanding the motion of satellites, spaceships, and other objects orbiting the Earth. Orbit Radius is denoted by r symbol.

How to calculate Circular Orbital Radius Given Velocity of Circular Orbit using this online calculator? To use this online calculator for Circular Orbital Radius Given Velocity of Circular Orbit, enter Velocity of Circular Orbit (vcir) and hit the calculate button. Here is how the Circular Orbital Radius Given Velocity of Circular Orbit calculation can be explained with given input values -> 11.07223 = [GM.Earth]/6050^2.

FAQ

What is Circular Orbital Radius Given Velocity of Circular Orbit?
Circular Orbital Radius Given Velocity of Circular Orbit formula is defined as the distance from the center of the Earth to an object in circular orbit, which is a critical parameter in understanding the motion of satellites, spaceships, and other objects orbiting the Earth and is represented as r = [GM.Earth]/vcir^2 or Orbit Radius = [GM.Earth]/Velocity of Circular Orbit^2. Velocity of Circular Orbit is the speed of a body in a circular orbit.
How to calculate Circular Orbital Radius Given Velocity of Circular Orbit?
Circular Orbital Radius Given Velocity of Circular Orbit formula is defined as the distance from the center of the Earth to an object in circular orbit, which is a critical parameter in understanding the motion of satellites, spaceships, and other objects orbiting the Earth is calculated using Orbit Radius = [GM.Earth]/Velocity of Circular Orbit^2. To calculate Circular Orbital Radius Given Velocity of Circular Orbit, you need Velocity of Circular Orbit (vcir). With our tool, you need to enter the respective value for Velocity of Circular Orbit and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
How many ways are there to calculate Orbit Radius?
In this formula, Orbit Radius uses Velocity of Circular Orbit. We can use 3 other way(s) to calculate the same, which is/are as follows -
  • Orbit Radius = Angular Momentum of Circular Orbit^2/[GM.Earth]
  • Orbit Radius = ((Time Period of Orbit*sqrt([GM.Earth]))/(2*pi))^(2/3)
  • Orbit Radius = -([GM.Earth])/(2*Specific Energy of Orbit)
Let Others Know
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!