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Parameter of Orbit Calculator

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The Two Body Problem

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✖Angular Momentum of Orbit is a fundamental physical quantity that characterizes the rotational motion of an object in orbit around a celestial body, such as a planet or a star.ⓘ Angular Momentum of Orbit [h]			+10% -10%
✖The Standard Gravitational Parameter of a celestial body is the product of the gravitational constant G and the mass M of the bodies.ⓘ Standard Gravitational Parameter [μ_std]			+10% -10%

✖Parameter of Orbit is defined as the half of chord length through the center of attraction perpendicular to the apse line.ⓘ Parameter of Orbit [p]

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Parameter of Orbit Solution

STEP 0: Pre-Calculation Summary

Formula Used

Parameter of Orbit = Angular Momentum of Orbit^2/Standard Gravitational Parameter
p = h^2/μ_std
This formula uses 3 Variables

Variables Used

Parameter of Orbit - (Measured in Meter) - Parameter of Orbit is defined as the half of chord length through the center of attraction perpendicular to the apse line.
Angular Momentum of Orbit - (Measured in Squaer Meter per Second) - Angular Momentum of Orbit is a fundamental physical quantity that characterizes the rotational motion of an object in orbit around a celestial body, such as a planet or a star.
Standard Gravitational Parameter - (Measured in Cubic Meter per Square Second) - The Standard Gravitational Parameter of a celestial body is the product of the gravitational constant G and the mass M of the bodies.

STEP 1: Convert Input(s) to Base Unit

Angular Momentum of Orbit: 65611 Square Kilometer per Second --> 65611000000 Squaer Meter per Second (Check conversion here)
Standard Gravitational Parameter: 398000000000000 Cubic Meter per Square Second --> 398000000000000 Cubic Meter per Square Second No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

p = h^2/μ_std --> 65611000000^2/398000000000000

Evaluating ... ...

p = 10816088.7462312

STEP 3: Convert Result to Output's Unit

10816088.7462312 Meter -->10816.0887462312 Kilometer (Check conversion here)

FINAL ANSWER

10816.0887462312 ≈ 10816.09 Kilometer <-- Parameter of Orbit

(Calculation completed in 00.006 seconds)

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Created by Karavadiya Divykumar Rasikbhai

Hindustan Institute of Technology and Science (HITS), Chennai, Indian

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Parameter of Orbit Formula

LaTeX Go

Parameter of Orbit = Angular Momentum of Orbit^2/Standard Gravitational Parameter
p = h^2/μ_std

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The semi-latus rectum is a parameter used to describe the size and shape of an ellipse in orbital mechanics. It is particularly important in the study of conic sections and Keplerian orbits.

How to Calculate Parameter of Orbit?

Parameter of Orbit calculator uses Parameter of Orbit = Angular Momentum of Orbit^2/Standard Gravitational Parameter to calculate the Parameter of Orbit, The Parameter of Orbit formula refers to a set of characteristics or properties that define the shape, size, orientation, and dynamics of an orbiting object's path around a central body. these parameters provide valuable information about the orbit and are essential for describing and analyzing the motion of objects in space. Parameter of Orbit is denoted by p symbol.

How to calculate Parameter of Orbit using this online calculator? To use this online calculator for Parameter of Orbit, enter Angular Momentum of Orbit (h) & Standard Gravitational Parameter (μ_std) and hit the calculate button. Here is how the Parameter of Orbit calculation can be explained with given input values -> 10.81609 = 65611000000^2/398000000000000.

FAQ

What is Parameter of Orbit?

The Parameter of Orbit formula refers to a set of characteristics or properties that define the shape, size, orientation, and dynamics of an orbiting object's path around a central body. these parameters provide valuable information about the orbit and are essential for describing and analyzing the motion of objects in space and is represented as p = h^2/μ_std or Parameter of Orbit = Angular Momentum of Orbit^2/Standard Gravitational Parameter. Angular Momentum of Orbit is a fundamental physical quantity that characterizes the rotational motion of an object in orbit around a celestial body, such as a planet or a star & The Standard Gravitational Parameter of a celestial body is the product of the gravitational constant G and the mass M of the bodies.

How to calculate Parameter of Orbit?

The Parameter of Orbit formula refers to a set of characteristics or properties that define the shape, size, orientation, and dynamics of an orbiting object's path around a central body. these parameters provide valuable information about the orbit and are essential for describing and analyzing the motion of objects in space is calculated using Parameter of Orbit = Angular Momentum of Orbit^2/Standard Gravitational Parameter. To calculate Parameter of Orbit, you need Angular Momentum of Orbit (h) & Standard Gravitational Parameter (μ_std). With our tool, you need to enter the respective value for Angular Momentum of Orbit & Standard Gravitational Parameter and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

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