Physical Nature Correction of the Second Focal Point in Keplerian Elliptical Orbits and a New Mechanism Interpretation
Classical astrophysics follows Kepler’s First Law, which describes planetary orbits as standard geometric ellipses with the Sun located at one focal point. It incorporates the second focal point as an inherent geometric feature of orbits, and has long confused mathematical models with real world physical mechanisms. Based on the energy storage steady state logic of the Light Origin Theory, this paper puts forward a core correction: planetary elliptical orbits are not governed by the geometric rule of dual focal points. The second focal point is merely a virtual reference generated by mathematical solutions and geometric plotting, carrying no physical entity. The non circular approximate elliptical orbits of solar system planets originate fundamentally from the bidirectional storage and dynamic conversion of kinetic and potential energy during orbital motion, which enables long term orbital stability. This paper also demonstrates that the eight planets of the Solar System share the Sun as their sole real physical focal point, whereas each planet corresponds to a virtual second focal point with a unique position, alongside distinct orbital curvature and eccentricity. This further proves that the second focal point possesses no physical reality. This energy storage steady state mechanism is generalizable to all gravitationally bound systems across the universe. It applies both to star planet systems and large scale galactic systems such as the Milky Way. Although these systems differ in scale, mass and motion parameters, they follow identical underlying physical principles. This paper clarifies fundamental logical loopholes in classical elliptical orbit theory and establishes a new orbit formation mechanism centred on energy steady state behaviour.
Authors
- Jiaqing Yan
Publication Details
- Journal
- Zenodo (CERN European Organization for Nuclear Research)
- Published
- 2026-08-17
- DOI
- https://doi.org/10.5281/zenodo.21981820
- Primary Topic
- Spacecraft Dynamics and Control
- Type
- preprint