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

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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. Check FAQs

v apogee = \frac{h e}{r e,apogee}

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

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

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

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

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

2.4253 = \frac{65750}{27110}

2.4253km/s = \frac{65750km²/s}{27110km}

2.4253 = \frac{65750}{27110}

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

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

FIRST Step Consider the formula

v apogee = \frac{h e}{r e,apogee}

Next Step Substitute values of Variables

∴

v apogee = \frac{65750km²/s}{27110km}

Next Step Convert Units

∴

v apogee = \frac{6.6E+10m²/s}{2.7E+7m}

Next Step Prepare to Evaluate

∴

v apogee = \frac{6.6E+10}{2.7E+7}

Next Step Evaluate

∴

v apogee = 2425.30431575065m/s

Next Step Convert to Output's Unit

∴

v apogee = 2.42530431575065km/s

LAST Step Rounding Answer

∴

v apogee = 2.4253km/s

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

Variables

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

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

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 Angular Momentum in Elliptic Orbit Given Apogee Radius and Apogee Velocity

h e = r e,apogee \cdot v apogee

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}

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

Apogee Velocity in Elliptic Orbit Given Angular Momentum and Apogee Radius evaluator uses Velocity of Satellite at Apogee = Angular Momentum of Elliptic Orbit/Apogee Radius in Elliptic Orbit to evaluate the Velocity of Satellite at Apogee, Apogee Velocity in Elliptic Orbit Given Angular Momentum and Apogee Radius formula is defined as the maximum velocity an object achieves in an elliptical orbit, which depends on the angular momentum and apogee radius of the orbit, providing crucial information for space mission design and celestial mechanics studies. Velocity of Satellite at Apogee is denoted by v_apogee symbol.

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

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

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

The formula of Apogee Velocity in Elliptic Orbit Given Angular Momentum and Apogee Radius is expressed as Velocity of Satellite at Apogee = Angular Momentum of Elliptic Orbit/Apogee Radius in Elliptic Orbit. Here is an example- 0.002425 = 65750000000/27110000.

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

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

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

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

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

Apogee Velocity in Elliptic Orbit Given Angular Momentum and Apogee Radius is usually measured using the Kilometer per Second[km/s] for Speed. Meter per Second[km/s], Meter per Minute[km/s], Meter per Hour[km/s] are the few other units in which Apogee Velocity in Elliptic Orbit Given Angular Momentum and Apogee Radius can be measured.

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

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

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

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

Other formulas in Elliptical Orbit Parameters category

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

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

Variable Name