Home Back

Bending Moment Of Beam Due To Stress In Steel Calculator

Formula Used:

\[ Eccentricity\ of\ Elliptical\ Orbit = \frac{Distance\ Between\ Two\ Foci}{2 \times Semi\ Major\ Axis\ of\ Elliptic\ Orbit} \] \[ e_e = \frac{d_{foci}}{2 \times a_e} \]

m
m

Unit Converter ▲

Unit Converter ▼

From: To:

1. What is the Eccentricity of Elliptical Orbit?

The Eccentricity of Elliptical Orbit is a measure of how stretched or elongated the orbit's shape is. It quantifies the deviation of the orbit from a perfect circle, with values ranging from 0 (circular) to values approaching 1 (highly elliptical).

2. How Does the Calculator Work?

The calculator uses the formula:

\[ e_e = \frac{d_{foci}}{2 \times a_e} \]

Where:

Explanation: The formula calculates the eccentricity by dividing the distance between the two foci by twice the semi-major axis of the elliptical orbit.

3. Importance of Eccentricity Calculation

Details: Calculating orbital eccentricity is crucial for understanding orbital mechanics, predicting satellite trajectories, and analyzing planetary motions in astronomy and aerospace engineering.

4. Using the Calculator

Tips: Enter the distance between two foci and the semi-major axis in meters. Both values must be positive numbers greater than zero for accurate calculation.

5. Frequently Asked Questions (FAQ)

Q1: What does an eccentricity value of 0 mean?
A: An eccentricity value of 0 indicates a perfect circular orbit where both foci coincide at the center.

Q2: What is the maximum possible value for eccentricity?
A: For elliptical orbits, eccentricity values range from 0 to values approaching 1 (but never reaching 1, which would be a parabolic orbit).

Q3: How does eccentricity affect orbital period?
A: For a given semi-major axis, eccentricity does not affect the orbital period according to Kepler's third law.

Q4: Can eccentricity be negative?
A: No, eccentricity is always a non-negative value between 0 and 1 for elliptical orbits.

Q5: How is eccentricity related to orbital energy?
A: For a given semi-major axis, orbits with higher eccentricity have the same total energy but different distributions between kinetic and potential energy throughout the orbit.

Bending Moment Of Beam Due To Stress In Steel Calculator© - All Rights Reserved 2025