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The table of eccentricities of the orbits published on Wikipedia does not show by what formulas the table is compiled.

Quote from: Yusup Hizirov on 23/06/2020 08:02:19The table of eccentricities of the orbits published on Wikipedia does not show by what formulas the table is compiled.What formula is used to measure a person's height?

To date, the eccentricities of planetary satellites are determined by trial and error,

because there are no formulas and methods for determining the eccentricities of orbits.

The solar Coriolis effect is involved in the formation of the orbits of the satellites of the planets. When the Moon revolving around the Earth in the fourth quarter approaches the Sun at a speed of 1 km / s, and in the second quarter moves away from the Sun at a speed of 1 km / s, the Coriolis Solar Force stretches the Moon’s orbit along the Earth’s orbit, thereby forming an ellipse of the Moon’s orbit. When the moon is in the phase of the new moon and the full moon, the solar Coriolis effect does not affect the orbit of the moon, because in these phases the moon does not approach and does not move away from the sun. The eccentricity of the lunar orbit varies from 0.044 to 0.072. https://en.m.wikipedia.org/wiki/Orbital_eccentricity The eccentricity of the orbit of the moon can be calculated by the following formula. E ≈ Vl / Vz.Vl - Orbital velocity of the moon.Vz - Orbital velocity of the Earth.The orbital speed of the moon is one revolution in 720 hours.The orbital speed of the Earth is one revolution in 8760 hours.E ≈ 720/8760 ≈ 0,082--------------The eccentricity of the orbit of the geostationary satellites can be calculated by the following formula. E ≈ Vi / VzWhere Vi is the satellite orbital velocity.Vz - Orbital velocity of the Earth.The satellite orbital speed is one revolution in 24 hours.The orbital speed of the Earth is one revolution in 8760 hours.E ≈ 24/8760 ≈ 0.0027-------------- Today, the eccentricity of planetary satellites is determined by trial and error, because, there are no formulas and methods for determining the eccentricity of orbits.http://www.sat.belastro.net/glava2/glava2.php#p1.2.cBased on the formula E ≈ Vl / Vz, it is possible to correct the distance from the Sun to the Earth, the orbital velocity of the Earth and the eccentricities of planetary satellites.https://en.m.wikipedia.org/wiki/Orbital_eccentricityThe statement that the elliptical orbit of the planets, the result of the disturbance of the planets is contrary to reality, because Venus moves almost in a circular orbit.The reason for the formation of the ellipse of the planets is in the task of three bodies. https://en.m.wikipedia.org/wiki/Three-body_problem

Interesting. Looks like the OP has removed some posts that make him look even more foolish than normal.

The formula E ≈ Vz / Vs shows that the Sun does not rotate around the center of the galaxy.

"Orbital velocity of the Sun" - one revolution in 250 million years.

he formula E ≈ Vz / Vs shows that the Sun does not rotate around the center of the galaxy.

The eccentricity of the Earth’s orbit can be calculated using the following formula. E ≈ Vz / Vs.Vz - Orbital velocity of the Earth.Vs - "Orbital velocity of the Sun."The orbital velocity of the Earth is one revolution in 1 year."Orbital velocity of the Sun" - one revolution in 250 million years.E ≈ 1/250,000,000 ≈ 0.00000000 ...

The stupider the hypothesis, the easier it is to refute it, provided that the opponent is not stupid!

The eccentricity of the planetary satellite orbit also depends on the physical libration of the satellites

the reason for which is in the three-body problem

The eccentricity of the orbit of the moon can be calculated by the formula. E = Vz: Ss / Vl: Sz = 0.076

E = Vz: Ss / Vl: Sz = 0.076

The eccentricity of the orbit of the moon varies from 0.044 to 0.072.

geological activity of the Earth

(Vz: Ss) / (Ve: Rz)

The coefficient of the geological activity of the Earth can be calculated by the formula. E = (Vz: Ss) / (Ve: Rz) = 0,00021Where Vz - Orbital velocity of the Earth - 8760 km / h.Ss - The distance between the Sun and the Earth is 150,000,000 km.Ve - Equatorial speed of rotation of the Earth: 1674 km / hRz - Radius of the Earth - 6,000 km.

The geological activity coefficient of Venus can be calculated by the formula. E ≈ Vэ / Vв = 0.0051Ve - Equatorial rotation speed of Venus - 0.18 km / s.Vв - Orbital velocity of Venus - 35 km / s.Coefficient of geological activity of the Earth. E ≈ Ve / Vz = 0.0155Ve - Equatorial speed of rotation of the Earth - 0.465 km / s.Vz - Orbital velocity of the Earth - 30 km / s.The coefficient of geological activity of Jupiter. E ≈ Vэ / Vю = 0.97Vе - Equatorial rotation speed of Jupiter - 12.6 km / s.Vю - The orbital velocity of Jupiter - 13 km / s.

The geological activity coefficient