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Angular Momentum of Trajectory given Parameter of Orbit Calculator

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✖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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✖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 Trajectory given Parameter of Orbit [h]

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Angular Momentum of Trajectory given Parameter of Orbit Solution

STEP 0: Pre-Calculation Summary

Formula Used

Angular Momentum of Orbit = sqrt(Parameter of Orbit*[GM.Earth])
h = sqrt(p*[GM.Earth])
This formula uses 1 Constants, 1 Functions, 2 Variables

Constants Used

[GM.Earth] - Earth’s Geocentric Gravitational Constant Value Taken As 3.986004418E+14

Functions Used

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., sqrt(Number)

Variables Used

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.
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.

STEP 1: Convert Input(s) to Base Unit

Parameter of Orbit: 10800 Kilometer --> 10800000 Meter (Check conversion here)

STEP 2: Evaluate Formula

Substituting Input Values in Formula

h = sqrt(p*[GM.Earth]) --> sqrt(10800000*[GM.Earth])

Evaluating ... ...

h = 65611620704.2624

STEP 3: Convert Result to Output's Unit

65611620704.2624 Squaer Meter per Second -->65611.6207042624 Square Kilometer per Second (Check conversion here)

FINAL ANSWER

65611.6207042624 ≈ 65611.62 Square Kilometer per Second <-- Angular Momentum of Orbit

(Calculation completed in 00.020 seconds)

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Angular Momentum of Trajectory given Parameter of Orbit Formula

LaTeX Go

Angular Momentum of Orbit = sqrt(Parameter of Orbit*[GM.Earth])
h = sqrt(p*[GM.Earth])

What is Trajectory ?

A trajectory is the path followed by an object as it moves through space, typically under the influence of external forces such as gravity, propulsion, or other interactions. It can refer to the motion of objects in various contexts, including physics, engineering, astronomy, and ballistics.

How to Calculate Angular Momentum of Trajectory given Parameter of Orbit?

Angular Momentum of Trajectory given Parameter of Orbit calculator uses Angular Momentum of Orbit = sqrt(Parameter of Orbit*[GM.Earth]) to calculate the Angular Momentum of Orbit, Angular Momentum of Trajectory given Parameter of Orbit refers to the rotational momentum of an orbiting object around the central body. It's a fundamental quantity in orbital mechanics and characterizes the motion of objects in orbit, this equation describes the magnitude of the angular momentum vector, which is conserved unless external torques act upon the orbiting object. Angular Momentum of Orbit is denoted by h symbol.

How to calculate Angular Momentum of Trajectory given Parameter of Orbit using this online calculator? To use this online calculator for Angular Momentum of Trajectory given Parameter of Orbit, enter Parameter of Orbit (p) and hit the calculate button. Here is how the Angular Momentum of Trajectory given Parameter of Orbit calculation can be explained with given input values -> 0.065612 = sqrt(10800000*[GM.Earth]).

FAQ

What is Angular Momentum of Trajectory given Parameter of Orbit?

Angular Momentum of Trajectory given Parameter of Orbit refers to the rotational momentum of an orbiting object around the central body. It's a fundamental quantity in orbital mechanics and characterizes the motion of objects in orbit, this equation describes the magnitude of the angular momentum vector, which is conserved unless external torques act upon the orbiting object and is represented as h = sqrt(p*[GM.Earth]) or Angular Momentum of Orbit = sqrt(Parameter of Orbit*[GM.Earth]). Parameter of Orbit is defined as the half of chord length through the center of attraction perpendicular to the apse line.

How to calculate Angular Momentum of Trajectory given Parameter of Orbit?

Angular Momentum of Trajectory given Parameter of Orbit refers to the rotational momentum of an orbiting object around the central body. It's a fundamental quantity in orbital mechanics and characterizes the motion of objects in orbit, this equation describes the magnitude of the angular momentum vector, which is conserved unless external torques act upon the orbiting object is calculated using Angular Momentum of Orbit = sqrt(Parameter of Orbit*[GM.Earth]). To calculate Angular Momentum of Trajectory given Parameter of Orbit, you need Parameter of Orbit (p). With our tool, you need to enter the respective value for Parameter of Orbit 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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