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Azimuth-Averaged Radius Given Apogee and Perigee Radii Formula

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Azimuth Averaged Radius is square root of the product of the maximum distance (apogee) and the minimum distance (perigee) from the focus of an elliptical orbit.. Check FAQs

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

r_θ - Azimuth Averaged Radius?r_e,apogee - Apogee Radius in Elliptic Orbit?r_e,perigee - Perigee Radius in Elliptic Orbit?

Azimuth-Averaged Radius Given Apogee and Perigee Radii Example

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Here is how the Azimuth-Averaged Radius Given Apogee and Perigee Radii equation looks like with Values.

Here is how the Azimuth-Averaged Radius Given Apogee and Perigee Radii equation looks like with Units.

Here is how the Azimuth-Averaged Radius Given Apogee and Perigee Radii equation looks like.

13555.5 = \sqrt{27110 \cdot 6778}

13555.5km = \sqrt{27110km \cdot 6778km}

13555.5 = \sqrt{27110 \cdot 6778}

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Azimuth-Averaged Radius Given Apogee and Perigee Radii Solution

Follow our step by step solution on how to calculate Azimuth-Averaged Radius Given Apogee and Perigee Radii?

FIRST Step Consider the formula

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

Next Step Substitute values of Variables

∴

r θ = \sqrt{27110km \cdot 6778km}

Next Step Convert Units

∴

r θ = \sqrt{2.7E+7m \cdot 6.8E+6m}

Next Step Prepare to Evaluate

∴

r θ = \sqrt{2.7E+7 \cdot 6.8E+6}

Next Step Evaluate

∴

r θ = 13555499.9907787m

Next Step Convert to Output's Unit

∴

r θ = 13555.4999907787km

LAST Step Rounding Answer

∴

r θ = 13555.5km

Azimuth-Averaged Radius Given Apogee and Perigee Radii Formula Elements

Variables

Functions

Azimuth Averaged Radius

Azimuth Averaged Radius is square root of the product of the maximum distance (apogee) and the minimum distance (perigee) from the focus of an elliptical orbit..

Symbol: r_θ

Measurement: LengthUnit: km

Note: Value should be greater than 0.

Formulas to find Azimuth Averaged Radius

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

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

sqrt

A square root function is a function that takes a non-negative number as an input and returns the square root of the given input number.

Syntax: sqrt(Number)

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 Azimuth-Averaged Radius Given Apogee and Perigee Radii?

Azimuth-Averaged Radius Given Apogee and Perigee Radii evaluator uses Azimuth Averaged Radius = sqrt(Apogee Radius in Elliptic Orbit*Perigee Radius in Elliptic Orbit) to evaluate the Azimuth Averaged Radius, Azimuth-Averaged Radius Given Apogee and Perigee Radii formula is defined as a measure of the average radius of an elliptical orbit at a given azimuth, providing a crucial parameter in understanding the shape and size of orbits in astronomy and space exploration. Azimuth Averaged Radius is denoted by r_θ symbol.

How to evaluate Azimuth-Averaged Radius Given Apogee and Perigee Radii using this online evaluator? To use this online evaluator for Azimuth-Averaged Radius Given Apogee and Perigee Radii, enter Apogee Radius in Elliptic Orbit (r_e,apogee) & Perigee Radius in Elliptic Orbit (r_e,perigee) and hit the calculate button.

FAQs on Azimuth-Averaged Radius Given Apogee and Perigee Radii

What is the formula to find Azimuth-Averaged Radius Given Apogee and Perigee Radii?

The formula of Azimuth-Averaged Radius Given Apogee and Perigee Radii is expressed as Azimuth Averaged Radius = sqrt(Apogee Radius in Elliptic Orbit*Perigee Radius in Elliptic Orbit). Here is an example- 13.5555 = sqrt(27110000*6778000).

How to calculate Azimuth-Averaged Radius Given Apogee and Perigee Radii?

With Apogee Radius in Elliptic Orbit (r_e,apogee) & Perigee Radius in Elliptic Orbit (r_e,perigee) we can find Azimuth-Averaged Radius Given Apogee and Perigee Radii using the formula - Azimuth Averaged Radius = sqrt(Apogee Radius in Elliptic Orbit*Perigee Radius in Elliptic Orbit). This formula also uses Square Root (sqrt) function(s).

Can the Azimuth-Averaged Radius Given Apogee and Perigee Radii be negative?

No, the Azimuth-Averaged Radius Given Apogee and Perigee Radii, measured in Length cannot be negative.

Which unit is used to measure Azimuth-Averaged Radius Given Apogee and Perigee Radii?

Azimuth-Averaged Radius Given Apogee and Perigee Radii is usually measured using the Kilometer[km] for Length. Meter[km], Millimeter[km], Decimeter[km] are the few other units in which Azimuth-Averaged Radius Given Apogee and Perigee Radii can be measured.

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Azimuth-Averaged Radius Given Apogee and Perigee Radii Formula

Azimuth-Averaged Radius Given Apogee and Perigee Radii Example

Azimuth-Averaged Radius Given Apogee and Perigee Radii Solution

Azimuth-Averaged Radius Given Apogee and Perigee Radii Formula Elements

Other formulas in Elliptical Orbit Parameters category

How to Evaluate Azimuth-Averaged Radius Given Apogee and Perigee Radii?

FAQs on Azimuth-Averaged Radius Given Apogee and Perigee Radii

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