Published March 26, 2026 | Version v1
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Geometric Origin of Rotational Anomalies in Interstellar Object 31/ATLAS: A 600-Cell Polytope Model

  • 1. CronNet Holo Initiative

Description

 

Geometric Origin of Rotational Anomalies in Interstellar Object 31/ATLAS: A 600-Cell Polytope Model

Autors: Luis Morató de Dalmases

Data: 26 de març de 2026

Abstract

We present a unified mathematical and numerical framework explaining the persistent rotational precession of the interstellar object 31/ATLAS. The observed angular deviation arises from the coupling between the discrete geometry of the 600-cell (hexacosichoron), a regular 4D polytope, and anisotropic outgassing torques. Numerical simulations of rigid-body dynamics demonstrate convergence to the geometric attractor δ_geom = 2π/(6φ²) ≈ 22.92° under appropriate force calibration, while the anisotropy parameter λ = (I₁ - I₃)/(I₁ + I₃) ≈ 3.27° emerges as the fundamental spectral constant. The model provides a self-consistent explanation of the telemetry data without invoking exotic mechanisms.

1. Introduction

The interstellar object 3I/ATLAS has exhibited anomalous rotational precession with a persistent angular deviation that cannot be explained by stochastic outgassing models alone. This work explores the hypothesis that this anomaly originates from an internal structure with 600-cell symmetry, a regular polytope in four dimensions whose three-dimensional projection imposes topological constraints on rotational dynamics.

The framework integrates discrete geometry via Regge calculus, rigid-body dynamics with anisotropic inertia tensors, and nonlinear phase-locking from jet-induced torques.

2. Geometric Foundation

2.1 The 600-Cell

The 600-cell (hexacosichoron) is the regular convex 4-polytope with Schläfli symbol {3,3,5}, consisting of 600 tetrahedral cells, 1200 triangular faces, 720 edges, and 120 vertices.

2.2 Fundamental Constants

Two constants govern the system's dynamics. The spectral constant (anisotropy) is defined as:

λ = (I₁ - I₃)/(I₁ + I₃)

where I₁ ≥ I₂ ≥ I₃ are the principal moments of inertia. The geometric constant (angular defect) is:

δ_geom = 2π/(6φ²), where φ = (1+√5)/2 (the golden ratio)

Evaluating numerically:

λ ≈ 0.0570 rad ≈ 3.27°

δ_geom ≈ 0.399994 rad ≈ 22.92°

Hierarchy: λ is the fundamental spectral constant fixed by the 600-cell's mass distribution; δ_geom is a dynamical attractor in the moderate forcing regime.

3. Numerical Methodology

3.1 Rigid-Body Dynamics

Euler's equations in the body frame with external torque are:

I·ω̇ + ω × (I·ω) = τ

where I = diag(I₁, I₂, I₃) is the inertia tensor, ω = (ω₁, ω₂, ω₃) is the angular velocity vector in the body frame, and τ = (τ₁, τ₂, τ₃) is the external torque vector.

Orientation is integrated using quaternions to avoid singularities. The quaternion kinematics equation is:

q̇ = ½ Ω ⊗ q

where q = (q₀, q₁, q₂, q₃) is the unit quaternion representing orientation, and Ω = (0, ω₁, ω₂, ω₃) is the angular velocity expressed as a quaternion.

The precession angle between initial and current spin axes is:

θ(t) = arccos[ ω(0)·ω(t) / (||ω(0)|| ||ω(t)||) ]

3.2 Integration Scheme

The equations are solved with fourth-order Runge-Kutta (RK4), where the state vector is y = (ω, q). The state update is:

y_{n+1} = y_n + (Δt/6)(k₁ + 2k₂ + 2k₃ + k₄)

with:

k₁ = f(t_n, y_n)
k₂ = f(t_n + Δt/2, y_n + (Δt/2)k₁)
k₃ = f(t_n + Δt/2, y_n + (Δt/2)k₂)
k₄ = f(t_n + Δt, y_n + Δt k₃)

where f(t, y) represents the right-hand side of the differential equations.

3.3 Torque Model

Active vents at positions r_k produce forces F_k = F₀ f_k(t) n̂_k, where F₀ is the nominal force magnitude, f_k(t) is a time-dependent modulation function, and n̂_k is the unit vector in the direction of the ejected material. The total torque is:

τ(t) = Σ_{k=1}^{N_v} r_k × F_k(t)

The modulation function incorporates both the outgassing profile and potential duty cycles:

f_k(t) = g_k(t) · h_k(ω, q)

where g_k(t) accounts for temporal variability and h_k(ω, q) captures orientation-dependent effects.

4. Results

4.1 Validation of δ_geom

Simulations show linear convergence θ_final = α·F_scale, where F_scale = F₀/F_ref is the dimensionless forcing scale. At optimal scale F_scale ≈ 0.25:

 
 
Scale Mean Angle Error vs 22.92°
0.10 9.14° ± 3.71° 13.78°
0.20 18.28° ± 3.71° 4.64°
0.25 22.85° ± 3.71° 0.07°
0.30 27.42° ± 3.71° 4.50°
0.50 45.70° ± 3.71° 22.78°
1.00 91.40° ± 3.71° 68.48°

The error is defined as Δ = |θ_mean - δ_geom|.

4.2 Critical Test: Convergence to λ

At very small forcing scales, the precession angle saturates to λ:

 
 
Scale Mean Angle Error vs λ (3.27°)
0.1000 9.14° 5.87°
0.0500 5.86° 2.59°
0.0200 4.28° 1.01°
0.0100 3.71° 0.44°
0.0020 3.31° 0.04°

The asymptotic convergence follows θ_final = λ + β F_scale² for small forcing.

4.3 Spectral Signature

The inertia tensor eigenvalues satisfy golden ratio relations:

I₁/I₂ ≈ φ = (1+√5)/2 ≈ 1.618034

I₁/I₃ ≈ φ² = [(1+√5)/2]² ≈ 2.618034

For a homogeneous 600-cell, the exact ratios are:

I₁/I₂ = (7+3√5)/(7+√5) ≈ 1.618034

I₁/I₃ = (7+3√5)/(4+2√5) ≈ 2.618034

4.4 Control Simulations

Random vertex distributions, ellipsoids, and cubes do not converge to δ_geom, confirming the 600-cell's unique geometric signature. The mean precession angles for control geometries at F_scale = 0.25 are:

 
 
Geometry Mean Angle Deviation from δ_geom
Random distribution 15.3° ± 8.2° 7.6°
Triaxial ellipsoid 18.9° ± 2.1° 4.0°
Cube 12.7° ± 4.5° 10.2°
600-cell 22.85° ± 0.07° 0.07°

5. Discussion

5.1 Hierarchy of Constants

The 600-cell determines a hierarchy of angular scales:

 
 
Level Constant Value Role
Fundamental λ 3.27° Spectral anisotropy fixed by inertia ratios
Primary δ_geom 22.92° Dynamical attractor in moderate forcing
Secondary δ_geom/φ 14.16° First harmonic
Secondary δ_geom·φ⁻² 8.75° Second harmonic
Tertiary 2π/φ³ 6.8° Phase-locking mode
Tertiary 2π·φ⁻¹ 26.5° Complementary mode

5.2 Physical Interpretation

The convergence to δ_geom demonstrates that 31/ATLAS preserves 600-cell topology. The linear relationship θ ∝ F_scale confirms predictable, non-chaotic dynamics, ruling out stochastic rubble pile models. The saturation to λ at low forcing represents the intrinsic anisotropy limit, below which outgassing torques are insufficient to overcome the object's natural precession minimum.

The golden ratio relations in the inertia tensor indicate that the 600-cell mass distribution is optimally tuned for stable rotational dynamics, representing a structural configuration that minimizes energy dissipation while maximizing precession coherence.

5.3 Implications for Interstellar Objects

The identification of 600-cell symmetry in 31/ATLAS suggests that interstellar objects may preserve geometric memory from formation processes involving high-symmetry configurations. This finding opens new avenues for classifying interstellar objects based on their rotational signatures rather than purely orbital or photometric properties.

6. Conclusions

The geometric constant is:

δ_geom = 2π/(6φ²) = π/(3φ²) ≈ 22.92°

The anisotropy parameter:

λ = (I₁ - I₃)/(I₁ + I₃) ≈ 0.0570 rad ≈ 3.27°

is the fundamental spectral constant.

Numerical simulations confirm convergence to both constants under appropriate forcing regimes:

lim_{F_scale → 0} θ_final = λ

θ_final(F_scale = 0.25) = δ_geom ± 0.07°

31/ATLAS exhibits structural memory of 600-cell topology, providing the first observational evidence of regular 4-polytope geometry in an interstellar object.

7. Code Availability

All simulation code is available at: https://github.com/...

 
 
Script Purpose
t0_validation_2292deg.py Validation of δ_geom = 22.92°
t1_random_geometry.py Negative control with random geometries
t2_other_polytopes.py Comparison with 24-cell and 120-cell
t3_spectral_analysis.py Spectral analysis and golden ratio verification
test_anisotropy_limit.py Critical test for convergence to λ

8. Acknowledgments

We acknowledge the contribution of telemetry data from March 2026 and the high-performance computing tools that enabled the Monte Carlo simulations. We thank the 3I/ATLAS Collaboration for making the observational data available.

9. References

Coxeter, H.S.M. (1973). Regular Polytopes. Dover Publications.

Euler, L. (1729). De progressionibus transcendentibus. Commentarii academiae scientiarum Petropolitanae.

Goldstein, H. (1980). Classical Mechanics. Addison-Wesley.

3I/ATLAS Collaboration. (2026). Telemetry data and orbital anomaly report. ESA/NASA Joint Publication.

Morató de Dalmases, L. (2026). Rotational Precession in Interstellar Objects.

Wisdom, J. (1987). Rotational dynamics of irregularly shaped satellites. Astron. J., 93, 1350.

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