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Apogee Heights Formula

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Apogee Height is the maximum height or distance above the Earth's surface that an object reaches in its orbit around the Earth. Check FAQs

H apogee = r apogee - [Earth-R]

H_apogee - Apogee Height?r_apogee - Apogee Radius?[Earth-R] - Earth mean radius?

Apogee Heights Example

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With units

Only example

Here is how the Apogee Heights equation looks like with Values.

Here is how the Apogee Heights equation looks like with Units.

Here is how the Apogee Heights equation looks like.

2476.9912 = 8848 - 6371.0088

2476.9912km = 8848km - 6371.0088km

2476.9912 = 8848 - 6371.0088

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Apogee Heights Solution

Follow our step by step solution on how to calculate Apogee Heights?

FIRST Step Consider the formula

H apogee = r apogee - [Earth-R]

Next Step Substitute values of Variables

∴

H apogee = 8848km - [Earth-R]

Next Step Substitute values of Constants

∴

H apogee = 8848km - 6371.0088km

Next Step Convert Units

∴

H apogee = 8.8E+6m - 6371.0088km

Next Step Prepare to Evaluate

∴

H apogee = 8.8E+6 - 6371.0088

Next Step Evaluate

∴

H apogee = 2476991.2m

LAST Step Convert to Output's Unit

∴

H apogee = 2476.9912km

Apogee Heights Formula Elements

Variables

Constants

Apogee Height

Apogee Height is the maximum height or distance above the Earth's surface that an object reaches in its orbit around the Earth.

Symbol: H_apogee

Measurement: LengthUnit: km

Note: Value should be greater than 0.

Formulas to find Apogee Height

Apogee Radius

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

Symbol: r_apogee

Measurement: LengthUnit: km

Note: Value should be greater than 0.

Formulas to find Apogee Radius

Earth mean radius

Earth mean radius represents the average distance from the Earth's center to any point on its surface, providing a single value to characterize the size of the Earth.

Symbol: [Earth-R]

Value: 6371.0088 km

Other formulas in Geostationary Orbit category

Go Angle of Elevation

∠θ el = ∠θ R - ∠θ tilt - λ e

Go Angle of Tilt

∠θ tilt = ∠θ R - ∠θ el - λ e

Go Satellite Geostationary Radius

R gso = {(\frac{[GM.Earth] \cdot P day}{4 \cdot π^{2}})}^{\frac{1}{3}}

Go Geostationary Height

H gso = R gso - [Earth-R]

How to Evaluate Apogee Heights?

Apogee Heights evaluator uses Apogee Height = Apogee Radius-[Earth-R] to evaluate the Apogee Height, Apogee Heights refers to the highest point in a satellite's elliptical orbit, where it moves slowest, facilitating efficient communication and longer visibility for ground stations during transmission. Apogee Height is denoted by H_apogee symbol.

How to evaluate Apogee Heights using this online evaluator? To use this online evaluator for Apogee Heights, enter Apogee Radius (r_apogee) and hit the calculate button.

FAQs on Apogee Heights

What is the formula to find Apogee Heights?

The formula of Apogee Heights is expressed as Apogee Height = Apogee Radius-[Earth-R]. Here is an example- 2.476991 = 8848000-[Earth-R].

How to calculate Apogee Heights?

With Apogee Radius (r_apogee) we can find Apogee Heights using the formula - Apogee Height = Apogee Radius-[Earth-R]. This formula also uses Earth mean radius constant(s).

Can the Apogee Heights be negative?

No, the Apogee Heights, measured in Length cannot be negative.

Which unit is used to measure Apogee Heights?

Apogee Heights is usually measured using the Kilometer[km] for Length. Meter[km], Millimeter[km], Decimeter[km] are the few other units in which Apogee Heights can be measured.

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