Angular Momentum of Trajectory given Parameter of Orbit Calculator

⤿

✖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]

+10%

-10%

✖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]

⎘ Copy

👎

Formula

✖

Angular Momentum of Trajectory given Parameter of Orbit

Formula

`"h" = sqrt("p"*"[GM.Earth]")`

Example

`"65611.62km²/s"=sqrt("10800km"*"[GM.Earth]")`

Calculator

LaTeX

Reset

👍

Download The Two Body Problem Formula PDF PDF Image

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 00.004 seconds)

You are here -

Home » Physics » Orbital Mechanics » The Two Body Problem » Fundamental Parameters » Angular Momentum of Trajectory given Parameter of Orbit

Credits

Created by Karavadiya Divykumar Rasikbhai

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

Karavadiya Divykumar Rasikbhai has created this Calculator and 10+ more calculators!

Verified by Kartikay Pandit

National Institute Of Technology (NIT), Hamirpur

Kartikay Pandit has verified this Calculator and 400+ more calculators!

< 8 Fundamental Parameters Calculators

Tsiolkovsky Rocket Equation

Go Change in Rocket Velocity = Specific Impulse*[g]*ln(Wet Mass/Dry mass)

Radius of Sphere of Influence( Black Hole)

Go Sphere of Influence Radius = [G.]*(Black Hole Mass)/(Stellar Velocity Dispersion of the Host Bulge)^2

Semi Major Axis of Phasing Ellipse

Go Semi Major Axis of Ellipse = ((Number of Periods*Gravitational Parameter^0.5)/(2*pi))^(2/3)

Radius of Sphere of Influence

Go Planet 2 radius = (Planet 1 radius/0.001)*(Planet 1 Mass/Planet 2 Mass)^(2/5)

Angular Momentum of Trajectory given Parameter of Orbit

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

Parameter of Orbit

Go Parameter of Orbit = Angular Momentum of Orbit^2/Standard Gravitational Parameter

Rocket Mass Ratio

Go Rocket Mass Ratio = e^(Change in Rocket Velocity/Rocket Exhaust Velocity)

Standard Gravitational Parameter

Go Standard Gravitational Parameter = [G.]*(Mass of Orbital Body 1)

Angular Momentum of Trajectory given Parameter of Orbit Formula

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

Why Parameter of Orbit is also known as Semi-latus rectum?

The latus rectum is the chord through the center of attraction perpendicular to the apse line. By symmetry, the center of attraction divides the latus rectum into two equal parts, each of length p, known historically as the semi-latus rectum. In modern parlance, p is called the parameter of the orbit.

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 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 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 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 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 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 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.

Home

FREE PDFs

🔍 Search