Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity Calculator

✖Perigee Radius in Elliptic Orbit 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 in Elliptic Orbit [r_e,perigee]			+10% -10%
✖Velocity of Satellite at Perigee is the velocity at which a satellite travels when it is at its closest point (perigee) to the celestial body it is orbiting, such as Earth.ⓘ Velocity of Satellite at Perigee [v_perigee]			+10% -10%

✖Angular Momentum of Elliptic 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 in Elliptic Orbit Given Perigee Radius and Perigee Velocity [h_e]

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Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity Solution

STEP 0: Pre-Calculation Summary

Formula Used

Angular Momentum of Elliptic Orbit = Perigee Radius in Elliptic Orbit*Velocity of Satellite at Perigee
h_e = r_e,perigee*v_perigee
This formula uses 3 Variables

Variables Used

Angular Momentum of Elliptic Orbit - (Measured in Squaer Meter per Second) - Angular Momentum of Elliptic 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.
Perigee Radius in Elliptic Orbit - (Measured in Meter) - Perigee Radius in Elliptic Orbit 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.
Velocity of Satellite at Perigee - (Measured in Meter per Second) - Velocity of Satellite at Perigee is the velocity at which a satellite travels when it is at its closest point (perigee) to the celestial body it is orbiting, such as Earth.

STEP 1: Convert Input(s) to Base Unit

Perigee Radius in Elliptic Orbit: 6778 Kilometer --> 6778000 Meter (Check conversion here)
Velocity of Satellite at Perigee: 9.7005 Kilometer per Second --> 9700.5 Meter per Second (Check conversion here)

STEP 2: Evaluate Formula

Substituting Input Values in Formula

h_e = r_e,perigee*v_perigee --> 6778000*9700.5

Evaluating ... ...

h_e = 65749989000

STEP 3: Convert Result to Output's Unit

65749989000 Squaer Meter per Second -->65749.989 Square Kilometer per Second (Check conversion here)

FINAL ANSWER

65749.989 ≈ 65749.99 Square Kilometer per Second <-- Angular Momentum of Elliptic Orbit

(Calculation completed in 00.004 seconds)

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

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< Elliptical Orbit Parameters Calculators

Eccentricity of Elliptical Orbit given Apogee and Perigee

LaTeX Go Eccentricity of Elliptical Orbit = (Apogee Radius in Elliptic Orbit-Perigee Radius in Elliptic Orbit)/(Apogee Radius in Elliptic Orbit+Perigee Radius in Elliptic Orbit)

Apogee Radius of Elliptic Orbit Given Angular Momentum and Eccentricity

LaTeX Go Apogee Radius in Elliptic Orbit = Angular Momentum of Elliptic Orbit^2/([GM.Earth]*(1-Eccentricity of Elliptical Orbit))

Semimajor Axis of Elliptic Orbit given Apogee and Perigee Radii

LaTeX Go Semi Major Axis of Elliptic Orbit = (Apogee Radius in Elliptic Orbit+Perigee Radius in Elliptic Orbit)/2

Angular Momentum in Elliptic Orbit Given Apogee Radius and Apogee Velocity

LaTeX Go Angular Momentum of Elliptic Orbit = Apogee Radius in Elliptic Orbit*Velocity of Satellite at Apogee

Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity Formula

LaTeX Go

Angular Momentum of Elliptic Orbit = Perigee Radius in Elliptic Orbit*Velocity of Satellite at Perigee
h_e = r_e,perigee*v_perigee

What is perigee Velocity ?

Perigee velocity is the velocity of an object at its perigee, which is the point in its orbit where it is closest to the central body it is orbiting, in orbital mechanics, the velocity of an object in orbit is not constant; it changes as the object moves along its elliptical path due to the influence of gravitational forces. At perigee, the object reaches its closest point to the central body and thus experiences its highest orbital velocity in its elliptical orbit.

How to Calculate Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity?

Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity calculator uses Angular Momentum of Elliptic Orbit = Perigee Radius in Elliptic Orbit*Velocity of Satellite at Perigee to calculate the Angular Momentum of Elliptic Orbit, Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity formula is defined as a measure of the tendency of an object to continue rotating or revolving around a central point in an elliptical orbit, dependent on the perigee radius and perigee velocity of the orbiting body. Angular Momentum of Elliptic Orbit is denoted by h_e symbol.

How to calculate Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity using this online calculator? To use this online calculator for Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity, enter Perigee Radius in Elliptic Orbit (r_e,perigee) & Velocity of Satellite at Perigee (v_perigee) and hit the calculate button. Here is how the Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity calculation can be explained with given input values -> 0.065747 = 6778000*9700.5.

FAQ

What is Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity?

Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity formula is defined as a measure of the tendency of an object to continue rotating or revolving around a central point in an elliptical orbit, dependent on the perigee radius and perigee velocity of the orbiting body and is represented as h_e = r_e,perigee*v_perigee or Angular Momentum of Elliptic Orbit = Perigee Radius in Elliptic Orbit*Velocity of Satellite at Perigee. Perigee Radius in Elliptic Orbit 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 & Velocity of Satellite at Perigee is the velocity at which a satellite travels when it is at its closest point (perigee) to the celestial body it is orbiting, such as Earth.

How to calculate Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity?

Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity formula is defined as a measure of the tendency of an object to continue rotating or revolving around a central point in an elliptical orbit, dependent on the perigee radius and perigee velocity of the orbiting body is calculated using Angular Momentum of Elliptic Orbit = Perigee Radius in Elliptic Orbit*Velocity of Satellite at Perigee. To calculate Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity, you need Perigee Radius in Elliptic Orbit (r_e,perigee) & Velocity of Satellite at Perigee (v_perigee). With our tool, you need to enter the respective value for Perigee Radius in Elliptic Orbit & Velocity of Satellite at Perigee 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 Angular Momentum of Elliptic Orbit?

In this formula, Angular Momentum of Elliptic Orbit uses Perigee Radius in Elliptic Orbit & Velocity of Satellite at Perigee. We can use 1 other way(s) to calculate the same, which is/are as follows -

Angular Momentum of Elliptic Orbit = Apogee Radius in Elliptic Orbit*Velocity of Satellite at Apogee

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