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True Anomaly of Asymptote in Hyperbolic Orbit given Eccentricity Formula

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The True Anomaly of Asymptote in Hyperbolic Orbit represents the angular measure of the position of an object within its hyperbolic trajectory relative to the asymptote. Check FAQs

θ inf = a \cos (- \frac{1}{e h})

θ_inf - True Anomaly of Asymptote in Hyperbolic Orbit?e_h - Eccentricity of Hyperbolic Orbit?

True Anomaly of Asymptote in Hyperbolic Orbit given Eccentricity Example

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Here is how the True Anomaly of Asymptote in Hyperbolic Orbit given Eccentricity equation looks like with Values.

Here is how the True Anomaly of Asymptote in Hyperbolic Orbit given Eccentricity equation looks like with Units.

Here is how the True Anomaly of Asymptote in Hyperbolic Orbit given Eccentricity equation looks like.

138.3162 = a \cos (- \frac{1}{1.339})

138.3162° = a \cos (- \frac{1}{1.339})

138.3162 = a \cos (- \frac{1}{1.339})

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True Anomaly of Asymptote in Hyperbolic Orbit given Eccentricity Solution

Follow our step by step solution on how to calculate True Anomaly of Asymptote in Hyperbolic Orbit given Eccentricity?

FIRST Step Consider the formula

θ inf = a \cos (- \frac{1}{e h})

Next Step Substitute values of Variables

∴

θ inf = a \cos (- \frac{1}{1.339})

Next Step Prepare to Evaluate

∴

θ inf = a \cos (- \frac{1}{1.339})

Next Step Evaluate

∴

θ inf = 2.41407271939116rad

Next Step Convert to Output's Unit

∴

θ inf = 138.316178258809°

LAST Step Rounding Answer

∴

θ inf = 138.3162°

True Anomaly of Asymptote in Hyperbolic Orbit given Eccentricity Formula Elements

Variables

Functions

True Anomaly of Asymptote in Hyperbolic Orbit

The True Anomaly of Asymptote in Hyperbolic Orbit represents the angular measure of the position of an object within its hyperbolic trajectory relative to the asymptote.

Symbol: θ_inf

Measurement: AngleUnit: °

Note: Value should be greater than 0.

Formulas to find True Anomaly of Asymptote in Hyperbolic Orbit

Eccentricity of Hyperbolic Orbit

Eccentricity of Hyperbolic Orbit describes how much the orbit differs from a perfect circle, and this value typically falls between 1 and infinity.

Symbol: e_h

Measurement: NAUnit: Unitless

Note: Value should be greater than 1.

Formulas to find Eccentricity of Hyperbolic Orbit

cos

Cosine of an angle is the ratio of the side adjacent to the angle to the hypotenuse of the triangle.

Syntax: cos(Angle)

acos

The inverse cosine function, is the inverse function of the cosine function. It is the function that takes a ratio as an input and returns the angle whose cosine is equal to that ratio.

Syntax: acos(Number)

Other formulas in Hperbolic Orbit Parameters category

Go Radial Position in Hyperbolic Orbit given Angular Momentum, True Anomaly, and Eccentricity

r h = \frac{{h h}^{2}}{[GM.Earth] \cdot (1 + e h \cdot \cos (θ))}

Go Perigee Radius of Hyperbolic Orbit given Angular Momentum and Eccentricity

r perigee = \frac{{h h}^{2}}{[GM.Earth] \cdot (1 + e h)}

Go Turn Angle given Eccentricity

δ = 2 \cdot a \sin (\frac{1}{e h})

Go Semi-Major Axis of Hyperbolic Orbit given Angular Momentum and Eccentricity

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

How to Evaluate True Anomaly of Asymptote in Hyperbolic Orbit given Eccentricity?

True Anomaly of Asymptote in Hyperbolic Orbit given Eccentricity evaluator uses True Anomaly of Asymptote in Hyperbolic Orbit = acos(-1/Eccentricity of Hyperbolic Orbit) to evaluate the True Anomaly of Asymptote in Hyperbolic Orbit, True Anomaly of Asymptote in Hyperbolic Orbit given Eccentricity formula is defined as a measure that describes the angle between the direction of the periapsis and the asymptote of a hyperbolic trajectory, influenced by the orbit's eccentricity. True Anomaly of Asymptote in Hyperbolic Orbit is denoted by θ_inf symbol.

How to evaluate True Anomaly of Asymptote in Hyperbolic Orbit given Eccentricity using this online evaluator? To use this online evaluator for True Anomaly of Asymptote in Hyperbolic Orbit given Eccentricity, enter Eccentricity of Hyperbolic Orbit (e_h) and hit the calculate button.

FAQs on True Anomaly of Asymptote in Hyperbolic Orbit given Eccentricity

What is the formula to find True Anomaly of Asymptote in Hyperbolic Orbit given Eccentricity?

The formula of True Anomaly of Asymptote in Hyperbolic Orbit given Eccentricity is expressed as True Anomaly of Asymptote in Hyperbolic Orbit = acos(-1/Eccentricity of Hyperbolic Orbit). Here is an example- 7924.933 = acos(-1/1.339).

How to calculate True Anomaly of Asymptote in Hyperbolic Orbit given Eccentricity?

With Eccentricity of Hyperbolic Orbit (e_h) we can find True Anomaly of Asymptote in Hyperbolic Orbit given Eccentricity using the formula - True Anomaly of Asymptote in Hyperbolic Orbit = acos(-1/Eccentricity of Hyperbolic Orbit). This formula also uses Cosine (cos), Inverse Cosine (acos) function(s).

Can the True Anomaly of Asymptote in Hyperbolic Orbit given Eccentricity be negative?

No, the True Anomaly of Asymptote in Hyperbolic Orbit given Eccentricity, measured in Angle cannot be negative.

Which unit is used to measure True Anomaly of Asymptote in Hyperbolic Orbit given Eccentricity?

True Anomaly of Asymptote in Hyperbolic Orbit given Eccentricity is usually measured using the Degree[°] for Angle. Radian[°], Minute[°], Second[°] are the few other units in which True Anomaly of Asymptote in Hyperbolic Orbit given Eccentricity can be measured.

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