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

GoAngular Momentum in Elliptic Orbit Given Apogee Radius and Apogee Velocity Formula

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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. Check FAQs

h e = r e,perigee \cdot v perigee

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

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

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Here is how the Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity equation looks like with Values.

Here is how the Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity equation looks like with Units.

Here is how the Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity equation looks like.

65749.989 = 6778 \cdot 9.7005

65749.989km²/s = 6778km \cdot 9.7005km/s

65749.989 = 6778 \cdot 9.7005

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

Follow our step by step solution on how to calculate Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity?

FIRST Step Consider the formula

h e = r e,perigee \cdot v perigee

Next Step Substitute values of Variables

∴

h e = 6778km \cdot 9.7005km/s

Next Step Convert Units

∴

h e = 6.8E+6m \cdot 9700.5m/s

Next Step Prepare to Evaluate

∴

h e = 6.8E+6 \cdot 9700.5

Next Step Evaluate

∴

h e = 65749989000m²/s

LAST Step Convert to Output's Unit

∴

h e = 65749.989km²/s

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

Variables

Angular Momentum of Elliptic Orbit

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.

Symbol: h_e

Measurement: Specific Angular MomentumUnit: km²/s

Note: Value should be greater than 0.

Formulas to find Angular Momentum of Elliptic Orbit

Perigee Radius in Elliptic Orbit

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.

Symbol: r_e,perigee

Measurement: LengthUnit: km

Note: Value should be greater than 0.

Formulas to find Perigee Radius in Elliptic Orbit

Velocity of Satellite at Perigee

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.

Symbol: v_perigee

Measurement: SpeedUnit: km/s

Note: Value should be greater than 0.

Formulas to find Velocity of Satellite at Perigee

Other Formulas to find Angular Momentum of Elliptic Orbit

Go Angular Momentum in Elliptic Orbit Given Apogee Radius and Apogee Velocity

h e = r e,apogee \cdot v apogee

Other formulas in Elliptical Orbit Parameters category

Go Eccentricity of Elliptical Orbit given Apogee and Perigee

e e = \frac{r e,apogee - r e,perigee}{r e,apogee + r e,perigee}

Go Apogee Radius of Elliptic Orbit Given Angular Momentum and Eccentricity

r e,apogee = \frac{{h e}^{2}}{[GM.Earth] \cdot (1 - e e)}

Go Semimajor Axis of Elliptic Orbit given Apogee and Perigee Radii

a e = \frac{r e,apogee + r e,perigee}{2}

Go Azimuth-Averaged Radius Given Apogee and Perigee Radii

r θ = \sqrt{r e,apogee \cdot r e,perigee}

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

Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity evaluator uses Angular Momentum of Elliptic Orbit = Perigee Radius in Elliptic Orbit*Velocity of Satellite at Perigee to evaluate 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 evaluate Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity using this online evaluator? To use this online evaluator 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.

FAQs on Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity

What is the formula to find Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity?

The formula of Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity is expressed as Angular Momentum of Elliptic Orbit = Perigee Radius in Elliptic Orbit*Velocity of Satellite at Perigee. Here is an example- 0.065747 = 6778000*9700.5.

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

With Perigee Radius in Elliptic Orbit (r_e,perigee) & Velocity of Satellite at Perigee (v_perigee) we can find Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity using the formula - Angular Momentum of Elliptic Orbit = Perigee Radius in Elliptic Orbit*Velocity of Satellite at Perigee.

What are the other ways to Calculate Angular Momentum of Elliptic Orbit?

Here are the different ways to Calculate Angular Momentum of Elliptic Orbit-

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

Can the Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity be negative?

No, the Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity, measured in Specific Angular Momentum cannot be negative.

Which unit is used to measure Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity?

Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity is usually measured using the Square Kilometer per Second[km²/s] for Specific Angular Momentum. Squaer Meter per Second[km²/s] are the few other units in which Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity can be measured.

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

​GoAngular Momentum in Elliptic Orbit Given Apogee Radius and Apogee Velocity Formula

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

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

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

Other Formulas to find Angular Momentum of Elliptic Orbit

Other formulas in Elliptical Orbit Parameters category

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

FAQs on Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity

Variable Name

GoAngular Momentum in Elliptic Orbit Given Apogee Radius and Apogee Velocity Formula