Perigee Radius of Hyperbolic Orbit given Angular Momentum and Eccentricity Calculator

✖Angular Momentum of Hyperbolic 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 Hyperbolic Orbit [h_h]			+10% -10%
✖Eccentricity of Hyperbolic Orbit describes how much the orbit differs from a perfect circle, and this value typically falls between 1 and infinity.ⓘ Eccentricity of Hyperbolic Orbit [e_h]			+10% -10%

✖Perigee Radius refers to the distance between the center of the Earth and the point in a satellite's orbit that is closest to the Earth's surface.ⓘ Perigee Radius of Hyperbolic Orbit given Angular Momentum and Eccentricity [r_perigee]

⎘ Copy

👎

Formula

LaTeX

Reset

👍

Download Hyperbolic Orbits Formulas PDF PDF Image

Perigee Radius of Hyperbolic Orbit given Angular Momentum and Eccentricity Solution

STEP 0: Pre-Calculation Summary

Formula Used

Perigee Radius = Angular Momentum of Hyperbolic Orbit^2/([GM.Earth]*(1+Eccentricity of Hyperbolic Orbit))
r_perigee = h_h^2/([GM.Earth]*(1+e_h))
This formula uses 1 Constants, 3 Variables

Constants Used

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

Variables Used

Perigee Radius - (Measured in Meter) - Perigee Radius refers to the distance between the center of the Earth and the point in a satellite's orbit that is closest to the Earth's surface.
Angular Momentum of Hyperbolic Orbit - (Measured in Squaer Meter per Second) - Angular Momentum of Hyperbolic 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.
Eccentricity of Hyperbolic Orbit - Eccentricity of Hyperbolic Orbit describes how much the orbit differs from a perfect circle, and this value typically falls between 1 and infinity.

STEP 1: Convert Input(s) to Base Unit

Angular Momentum of Hyperbolic Orbit: 65700 Square Kilometer per Second --> 65700000000 Squaer Meter per Second (Check conversion here)
Eccentricity of Hyperbolic Orbit: 1.339 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

r_perigee = h_h^2/([GM.Earth]*(1+e_h)) --> 65700000000^2/([GM.Earth]*(1+1.339))

Evaluating ... ...

r_perigee = 4629805.44742964

STEP 3: Convert Result to Output's Unit

4629805.44742964 Meter -->4629.80544742964 Kilometer (Check conversion here)

FINAL ANSWER

4629.80544742964 ≈ 4629.805 Kilometer <-- Perigee Radius

(Calculation completed in 00.004 seconds)

You are here -

Home » Physics » Orbital Mechanics » The Two Body Problem » Hyperbolic Orbits » Aerospace » Hperbolic Orbit Parameters » Perigee Radius of Hyperbolic Orbit given Angular Momentum and Eccentricity

Credits

Created by Harsh Raj

Indian Institute of Technology, Kharagpur (IIT KGP), West Bengal

Harsh Raj has created this Calculator and 50+ more calculators!

Verified by Kartikay Pandit

National Institute Of Technology (NIT), Hamirpur

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

< Hperbolic Orbit Parameters Calculators

Radial Position in Hyperbolic Orbit given Angular Momentum, True Anomaly, and Eccentricity

LaTeX Go Radial Position in Hyperbolic Orbit = Angular Momentum of Hyperbolic Orbit^2/([GM.Earth]*(1+Eccentricity of Hyperbolic Orbit*cos(True Anomaly)))

Semi-Major Axis of Hyperbolic Orbit given Angular Momentum and Eccentricity

LaTeX Go Semi Major Axis of Hyperbolic Orbit = Angular Momentum of Hyperbolic Orbit^2/([GM.Earth]*(Eccentricity of Hyperbolic Orbit^2-1))

Perigee Radius of Hyperbolic Orbit given Angular Momentum and Eccentricity

LaTeX Go Perigee Radius = Angular Momentum of Hyperbolic Orbit^2/([GM.Earth]*(1+Eccentricity of Hyperbolic Orbit))

Turn Angle given Eccentricity

LaTeX Go Turn Angle = 2*asin(1/Eccentricity of Hyperbolic Orbit)

Perigee Radius of Hyperbolic Orbit given Angular Momentum and Eccentricity Formula

LaTeX Go

Perigee Radius = Angular Momentum of Hyperbolic Orbit^2/([GM.Earth]*(1+Eccentricity of Hyperbolic Orbit))
r_perigee = h_h^2/([GM.Earth]*(1+e_h))

What is Gravitational Attraction ?

Gravitational attraction refers to the force of attraction between two objects with mass due to gravity. This force is described by Isaac Newton's law of universal gravitation, which states that every particle of matter in the universe attracts every other particle with a force that is directly proportional to the product of their masses and inversely proportional to the square of the distance between their centers.

How to Calculate Perigee Radius of Hyperbolic Orbit given Angular Momentum and Eccentricity?

Perigee Radius of Hyperbolic Orbit given Angular Momentum and Eccentricity calculator uses Perigee Radius = Angular Momentum of Hyperbolic Orbit^2/([GM.Earth]*(1+Eccentricity of Hyperbolic Orbit)) to calculate the Perigee Radius, Perigee Radius of Hyperbolic Orbit given Angular Momentum and Eccentricity formula is defined as a method to determine the closest distance of a hyperbolic orbiting body to the central mass, based on its angular momentum and eccentricity. Perigee Radius is denoted by r_perigee symbol.

How to calculate Perigee Radius of Hyperbolic Orbit given Angular Momentum and Eccentricity using this online calculator? To use this online calculator for Perigee Radius of Hyperbolic Orbit given Angular Momentum and Eccentricity, enter Angular Momentum of Hyperbolic Orbit (h_h) & Eccentricity of Hyperbolic Orbit (e_h) and hit the calculate button. Here is how the Perigee Radius of Hyperbolic Orbit given Angular Momentum and Eccentricity calculation can be explained with given input values -> 4.629805 = 65700000000^2/([GM.Earth]*(1+1.339)).

FAQ

What is Perigee Radius of Hyperbolic Orbit given Angular Momentum and Eccentricity?

Perigee Radius of Hyperbolic Orbit given Angular Momentum and Eccentricity formula is defined as a method to determine the closest distance of a hyperbolic orbiting body to the central mass, based on its angular momentum and eccentricity and is represented as r_perigee = h_h^2/([GM.Earth]*(1+e_h)) or Perigee Radius = Angular Momentum of Hyperbolic Orbit^2/([GM.Earth]*(1+Eccentricity of Hyperbolic Orbit)). Angular Momentum of Hyperbolic 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 & Eccentricity of Hyperbolic Orbit describes how much the orbit differs from a perfect circle, and this value typically falls between 1 and infinity.

How to calculate Perigee Radius of Hyperbolic Orbit given Angular Momentum and Eccentricity?

Perigee Radius of Hyperbolic Orbit given Angular Momentum and Eccentricity formula is defined as a method to determine the closest distance of a hyperbolic orbiting body to the central mass, based on its angular momentum and eccentricity is calculated using Perigee Radius = Angular Momentum of Hyperbolic Orbit^2/([GM.Earth]*(1+Eccentricity of Hyperbolic Orbit)). To calculate Perigee Radius of Hyperbolic Orbit given Angular Momentum and Eccentricity, you need Angular Momentum of Hyperbolic Orbit (h_h) & Eccentricity of Hyperbolic Orbit (e_h). With our tool, you need to enter the respective value for Angular Momentum of Hyperbolic Orbit & Eccentricity of Hyperbolic 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