USP Field Theory – Universal Orbital Mechanics Equation

This release presents the full USP Field Theory Universal Orbital Mechanics Equation, providing a unified framework for modeling the orbits of planets, moons, and artificial satellites without per-object adjustments or epoch-specific corrections. In USP Field Theory, gravity is reinterpreted as a spin-tension gradient in the ultra-sub particle (USP) field, directly linked to atomic-core density, planetary radius, and rotation rate. This approach eliminates empirical “fudge factors” and maintains predictive accuracy across time and different celestial bodies. Contents include: Step-by-step derivation of the Master Orbital Equation. Definition of all parameters and their USP-specific interpretations. Worked examples for Earth, Mercury, and Jupiter. Verification against historical data. Predictive applications for planetary systems, satellites, and asteroids. Computational framework and precomputed core density/volume tables. This model is applicable to both planetary and artificial orbital planning, providing long-term stability predictions in any gravitational environment.

Publication Details

Journal
Zenodo (CERN European Organization for Nuclear Research)
Published
2025-08-09
DOI
https://doi.org/10.5281/zenodo.16785861
Primary Topic
Patient Satisfaction in Healthcare
Type
article
Field-Weighted Citation Impact
0.00
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article

USP Field Theory – Universal Orbital Mechanics Equation

Zenodo (CERN European Organization for Nuclear Research)
Patient Satisfaction in Healthcare
article

USP Field Theory – Universal Orbital Mechanics Equation

article en

Abstract

This release presents the full USP Field Theory Universal Orbital Mechanics Equation, providing a unified framework for modeling the orbits of planets, moons, and artificial satellites without per-object adjustments or epoch-specific corrections. In USP Field Theory, gravity is reinterpreted as a spin-tension gradient in the ultra-sub particle (USP) field, directly linked to atomic-core density, planetary radius, and rotation rate. This approach eliminates empirical “fudge factors” and maintains predictive accuracy across time and different celestial bodies. Contents include: Step-by-step derivation of the Master Orbital Equation. Definition of all parameters and their USP-specific interpretations. Worked examples for Earth, Mercury, and Jupiter. Verification against historical data. Predictive applications for planetary systems, satellites, and asteroids. Computational framework and precomputed core density/volume tables. This model is applicable to both planetary and artificial orbital planning, providing long-term stability predictions in any gravitational environment.

Zenodo (CERN European Organization for Nuclear Research)
Openalex Percentile: Top 38%
Patient Satisfaction in Healthcare
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