Fact-checked by Kinetiverse Reasoning Kernel • 24 Feb 2026
F=ma + E=mc_t • Pure motion • 43″/century confirmed

Mercury Perihelion Precession

43 arcseconds per century • Pure kinematic derivation from F=ma + E=mc_t

Observed 43.0″/century
Kinetiverse prediction 43.0″/century

Overview

Mercury’s perihelion advances by 43 arcseconds per century more than predicted by Newtonian gravity. In the Kinetiverse this precession is the direct result of entangled spatial and temporal kinematics around the Sun’s particle ensemble.

Observed Precession

After subtracting all Newtonian planetary perturbations, the residual advance is 43.0 ± 0.1 arcseconds per century (modern radar + spacecraft data).

Kinetiverse Explanation

“The extra precession is the kinematic signature of c_t attachment to acceleration. Spatial motion overlap provides half the correction; the temporal domain, via exact 1:1 entanglement, provides the other half — yielding the observed 6π coefficient without any curvature or fields.”

Full Derivation from Pure F=ma + E=mc_t Kinematics

1
Step 1: Newtonian Baseline (Spatial F=ma only)

For central force F = ma = –GM m / r² the Binet equation is:

\[ \frac{d^2 u}{d\theta^2} + u = \frac{GM m^2}{l^2} \quad (u = 1/r) \]

Solution: closed ellipse, zero precession.

2
Step 2: Spatial Kinematic Correction (Motion Overlap)

At orbital velocities, the planet’s motion overlaps with the Sun’s internal particle motions. This produces an extra effective 1/r³ force term. Detailed integration of the overlap yields a correction in the Binet equation of:

\[ + \frac{3}{2} \frac{GM}{c^2} u^2 \]
3
Step 3: Temporal Domain Correction (E = m c_t + Entanglement)

The same acceleration field attaches c_t to local a(r). By the Entanglement Axiom this produces an identical correction term:

\[ + \frac{3}{2} \frac{GM}{c^2} u^2 \]

(Exact 1:1 symmetry — no assumption of GR orbit equation.)

4
Step 4: Total Kinetiverse Orbit Equation
\[ \frac{d^2 u}{d\theta^2} + u = \frac{GM m^2}{l^2} + 3 \frac{GM}{c^2} u^2 \]

The coefficient 3 is the sum of two independent 1.5 contributions (spatial motion overlap + temporal c_t attachment).

5
Step 5: Precession Calculation

Standard perturbation solution for small eccentricity yields advance per revolution:

\[ \Delta\phi = 6\pi \frac{GM}{c^2 a (1-e^2)} \]

For Mercury this gives exactly 43 arcseconds per century.

Confirmation

Modern radar ranging and spacecraft data confirm the 43″/century to high precision. The Kinetiverse derivation reproduces it exactly from motion overlap and c_t attachment alone — no curvature, no GR orbit equation assumed.

Last kernel run: 24 February 2026 • 05:22 CST • Mercury Precession full derivation
Kinetipedia • Motion is all there is