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

GoAngular Momentum in Elliptic Orbit Given Perigee Radius and Perigee 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,apogee \cdot v apogee

h_e - Angular Momentum of Elliptic Orbit?r_e,apogee - Apogee Radius in Elliptic Orbit?v_apogee - Velocity of Satellite at Apogee?

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

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

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

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

65750 = 27110 \cdot 2.4253

65750km²/s = 27110km \cdot 2.4253km/s

65750 = 27110 \cdot 2.4253

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

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

FIRST Step Consider the formula

h e = r e,apogee \cdot v apogee

Next Step Substitute values of Variables

∴

h e = 27110km \cdot 2.4253km/s

Next Step Convert Units

∴

h e = 2.7E+7m \cdot 2425.3043m/s

Next Step Prepare to Evaluate

∴

h e = 2.7E+7 \cdot 2425.3043

Next Step Evaluate

∴

h e = 65750000006.76m²/s

Next Step Convert to Output's Unit

∴

h e = 65750.00000676km²/s

LAST Step Rounding Answer

∴

h e = 65750km²/s

Angular Momentum in Elliptic Orbit Given Apogee Radius and Apogee 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

Apogee Radius in Elliptic Orbit

Apogee Radius in Elliptic Orbit represents the maximum distance between an orbiting body and the object it orbits.

Symbol: r_e,apogee

Measurement: LengthUnit: km

Note: Value should be greater than 0.

Formulas to find Apogee Radius in Elliptic Orbit

Velocity of Satellite at Apogee

Velocity of Satellite at Apogee refers to the speed at which a satellite travels when it is at its farthest point from the celestial body it is orbiting, such as Earth.

Symbol: v_apogee

Measurement: SpeedUnit: km/s

Note: Value should be greater than 0.

Formulas to find Velocity of Satellite at Apogee

Other Formulas to find Angular Momentum of Elliptic Orbit

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

h e = r e,perigee \cdot v perigee

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 Apogee Radius and Apogee Velocity?

Angular Momentum in Elliptic Orbit Given Apogee Radius and Apogee Velocity evaluator uses Angular Momentum of Elliptic Orbit = Apogee Radius in Elliptic Orbit*Velocity of Satellite at Apogee to evaluate the Angular Momentum of Elliptic Orbit, Angular Momentum in Elliptic Orbit Given Apogee Radius and Apogee Velocity formula is defined as a measure of the tendency of an object to resist changes in its rotational motion as it orbits around a central body in an elliptical path. Angular Momentum of Elliptic Orbit is denoted by h_e symbol.

How to evaluate Angular Momentum in Elliptic Orbit Given Apogee Radius and Apogee Velocity using this online evaluator? To use this online evaluator for Angular Momentum in Elliptic Orbit Given Apogee Radius and Apogee Velocity, enter Apogee Radius in Elliptic Orbit (r_e,apogee) & Velocity of Satellite at Apogee (v_apogee) and hit the calculate button.

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

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

The formula of Angular Momentum in Elliptic Orbit Given Apogee Radius and Apogee Velocity is expressed as Angular Momentum of Elliptic Orbit = Apogee Radius in Elliptic Orbit*Velocity of Satellite at Apogee. Here is an example- 0.065606 = 27110000*2425.304316.

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

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

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=Perigee Radius in Elliptic Orbit*Velocity of Satellite at Perigee

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

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

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

Angular Momentum in Elliptic Orbit Given Apogee Radius and Apogee 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 Apogee Radius and Apogee Velocity can be measured.

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

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

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

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

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

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

Variable Name

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