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New Theories / Re: The Coriolis Force on Earth and in the Universe
« on: 08/07/2020 07:39:33 »The eccentricity of the orbit of the moon can be calculated by the following formula. E ≈ Vz / Vl = 30/360 = 0,083Satellites that are in resonance between themselves and with the planet, as a rule, move stably and move away from the planet.
Where Vz - Orbital velocity of the Earth - 30 degrees / month.
Vl - Orbital velocity of the moon - 360 degrees / month.
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The eccentricity of the orbit of the moon can be calculated by the following formula.
E ≈ (Vz / Sz) / (Vl / Sl) = 0.00071 / 0.0095 = 0.074
Where Vz - Orbital velocity of the Earth - 107 000 km / h.
Sz - Distance from the Sun to the Earth - 150,000,000
Where Vl - Orbital velocity of the moon - 3680 km / h.
Sl - Distance from the Earth to the Moon 384 000км.
The eccentricity of the orbit of the moon varies, from 0.026 to 0.077.
And satellites that do not resonate with the planet move randomly, somersault, change eccentricity and approach the planet.
The eccentricity of satellites is also affected by the physical libration of planetary satellites, the nature of which is in the three-body problem.