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πŸ“„ Fibonacci Laws β€” Read the paper
ReferenceFibonacci Laws Derivation

Fibonacci Laws of Planetary Motion β€” Technical Background

Looking for the accessible version? See Fibonacci Laws for a plain-language overview of what the six laws predict and why they matter. This page contains the full technical derivation.

What this page shows

Every planet has two key orbital properties that change slowly over hundreds of thousands of years:

  • Eccentricity β€” how elongated the orbit is (0 = perfect circle, 1 = extreme ellipse). Earth’s is currently about 0.017, meaning its orbit is nearly circular.
  • Inclination β€” how tilted the orbit is relative to the average plane of the Solar System. All planets wobble up and down slightly over long timescales; the oscillation amplitude measures how far each planet tilts.

When each value is multiplied by m\sqrt{m} (where mm is the planet’s mass), both eccentricities and inclinations snap onto Fibonacci ratios across all eight planets. The m\sqrt{m} weighting is not arbitrary β€” it is the unique exponent that arises in the Angular Momentum Deficit (AMD), the conserved quantity governing long-term orbital stability. In AMD-natural variables (ΞΎ=em\xi = e\sqrt{m} for eccentricity, Ξ·=im\eta = i\sqrt{m} for inclination), ratios between planets become simple Fibonacci fractions.

The six laws documented below are:

  1. Law 1 β€” Fibonacci Cycle Hierarchy: dividing HH by successive Fibonacci numbers yields the major precession periods
  2. Law 2 β€” Inclination constant: dΓ—ampΓ—m=ψd \times \text{amp} \times \sqrt{m} = \psi with a single universal constant ψ\psi and pure Fibonacci divisors dd
  3. Law 3 β€” Inclination balance: angular-momentum-weighted amplitudes cancel between two phase groups (99.9998% balance)
  4. Law 4 β€” Eccentricity constant: AMD partition ratios satisfy two Fibonacci constraints per mirror pair, determining all 8 eccentricities (0 free parameters)
  5. Law 5 β€” Eccentricity balance: an independent balance condition on eccentricities using the same divisors and phase groups (99.88% balance)
  6. Law 6 β€” Saturn-Jupiter-Earth Resonance: a closed beat-frequency loop linking the three dominant precession periods

The universal constant ψ\psi can be computed purely from Fibonacci numbers and the Holistic-Year H=333,888H = 333{,}888:

ψ=F5Γ—F822H=2205667,776=3.302Γ—10βˆ’3\psi = \frac{F_5 \times F_8^2}{2H} = \frac{2205}{667{,}776} = 3.302 \times 10^{-3}

From this single constant, all eight planets’ inclination amplitudes are predicted with zero free parameters. Combined with the eccentricity laws, the model connects orbital shapes and tilts of all eight planets through Fibonacci arithmetic rooted in a single timescale β€” the Holistic-Year H=333,888H = 333{,}888 years, which also determines each planet’s precession period (Law 1; see also Precession).

Prediction summary

Precession periods β€” Law 1 shows that dividing HH by successive Fibonacci numbers yields all major precession periods. The beat frequency rule 1/H(n)+1/H(n+1)=1/H(n+2)1/H(n) + 1/H(n+1) = 1/H(n+2) is an algebraic identity from the Fibonacci recurrence.

Inclination amplitudes β€” predicted from the single ψ=2205/(2H)\psi = 2205/(2H) with pure Fibonacci divisors. All 8 planets fit within their Laplace-Lagrange secular theory bounds. The configuration is the unique solution (Config #32) satisfying all four physical constraints out of 7,558,272 tested β€” see Law 2 and Finding 2 for details.

All eight eccentricities β€” Law 4 predicts all eccentricities from inclinations via Fibonacci pair constraints on the AMD partition ratio, with zero free parameters. Inner planets also form a Fibonacci ladder ΞΎV:ΞΎE:ΞΎMa:ΞΎMe=1:5/2:5:8\xi_V : \xi_E : \xi_{\text{Ma}} : \xi_{\text{Me}} = 1 : 5/2 : 5 : 8, where ΞΎ=eΓ—m\xi = e \times \sqrt{m}. See Law 4 and Finding 5 for details.

Predictive system status

ParameterFree parametersPlanets predictedAccuracy
Precession periods0 (from HH / Fibonacci)6 cyclesexact (algebraic identity)
Inclination0 (from HH + balance condition)8 of 8all within LL bounds
Eccentricity0 (from R2R^2 partition + inclinations)8 of 8all within 3%
Resonance loop0 (from Fibonacci addition)3 periodsexact (algebraic identity)

Input Data

Masses and semi-major axes are derived from the Holistic computation chain (H=333,888H = 333{,}888, orbit counts, Kepler’s third law). Eccentricities are J2000 values except Earth, where the oscillation-midpoint base eccentricity (0.015321) from the 3D simulation is used β€” see Finding 5. Inclinations are to the invariable plane at J2000 (Souami & Souchay 2012). Inclination amplitudes are derived from the Fibonacci formula amp=ψ/(dΓ—m)\text{amp} = \psi / (d \times \sqrt{m}).

PlanetMass (MβŠ™M_\odot)m\sqrt{m}aa (AU)eeii J2000 (Β°)Ξ©\Omega J2000 (Β°)
Mercury1.660Γ—10βˆ’71.660 \times 10^{-7}4.074Γ—10βˆ’44.074 \times 10^{-4}0.38710.20566.347332.83
Venus2.448Γ—10βˆ’62.448 \times 10^{-6}1.564Γ—10βˆ’31.564 \times 10^{-3}0.72330.00682.154554.70
Earth3.003Γ—10βˆ’63.003 \times 10^{-6}1.733Γ—10βˆ’31.733 \times 10^{-3}1.00000.01531.5787284.51
Mars3.227Γ—10βˆ’73.227 \times 10^{-7}5.681Γ—10βˆ’45.681 \times 10^{-4}1.52370.09341.6312354.87
Jupiter9.548Γ—10βˆ’49.548 \times 10^{-4}3.090Γ—10βˆ’23.090 \times 10^{-2}5.19970.04840.3220312.89
Saturn2.859Γ—10βˆ’42.859 \times 10^{-4}1.691Γ—10βˆ’21.691 \times 10^{-2}9.53060.05390.9255118.81
Uranus4.366Γ—10βˆ’54.366 \times 10^{-5}6.608Γ—10βˆ’36.608 \times 10^{-3}19.1380.04730.9947307.80
Neptune5.151Γ—10βˆ’55.151 \times 10^{-5}7.177Γ—10βˆ’37.177 \times 10^{-3}29.9600.00860.7354192.04

Assignments

Planet Configuration

PlanetPeriod (yr)Period =ddFibonacciPhase
Mercury242,828H/(11/8)H/(11/8)21F8F_8203Β°
Venus667,7762H2H34F9F_9203Β°
Earth111,296H/3H/33F4F_4203Β°
Mars77,051H/(13/3)H/(13/3)5F5F_5203Β°
Jupiter66,778H/5H/55F5F_5203Β°
Saturn41,736H/8H/83F4F_423Β°
Uranus111,296H/3H/321F8F_8203Β°
Neptune667,7762H2H34F9F_9203Β°

Phase Groups

The model uses two phase angles, 180Β° apart, derived from the s8s_8 eigenmode of Laplace-Lagrange secular perturbation theory (Ξ³8β‰ˆ203.3195Β°\gamma_8 \approx 203.3195Β°):

Phase anglePlanets
203.3195Β°Mercury, Venus, Earth, Mars, Jupiter, Uranus, Neptune
23.3195Β°Saturn (retrograde, solo)

The group assignment is constrained by: (1) each planet’s oscillation range must fall within the Laplace-Lagrange secular theory bounds, (2) the inclination structural weights must balance (Law 3), and (3) the eccentricity weights must balance (Law 5).

Inclination phase groups on the invariable plane: seven planets (prograde, 203Β°) balanced against Saturn alone (retrograde, 23Β°)

Precession Periods

PlanetPeriod (years)Expression
Mercury242,8288H/118H/11
Venus667,7762H2H
Earth111,296H/3H/3
Mars77,0513H/133H/13
Jupiter66,778H/5H/5
Saturnβˆ’41,736-41{,}736βˆ’H/8-H/8 (retrograde)
Uranus111,296H/3H/3
Neptune667,7762H2H

Paired planets: Earth and Uranus share the same period (H/3H/3). Venus and Neptune share the same period (2H2H). These pairings β€” one inner planet mirrored by one outer planet β€” also appear in the mirror-symmetric Fibonacci divisor assignments.


Law 1: The Fibonacci Cycle Hierarchy

Dividing the Holistic-Year H=333,888H = 333{,}888 by successive Fibonacci numbers yields the major precession periods of the solar system.

T(n)=H/FnT(n) = H / F_n
Fibonacci FnF_nH/FnH / F_nPeriod (years)Astronomical meaning
F4=3F_4 = 3H/3H/3111,296Earth true perihelion precession
F5=5F_5 = 5H/5H/566,778Jupiter perihelion precession
F6=8F_6 = 8H/8H/841,736Saturn perihelion precession (retrograde)
F7=13F_7 = 13H/13H/1325,684Axial precession
F8=21F_8 = 21H/21H/2115,899Saturn + Axial beat frequency
F9=34F_9 = 34H/34H/349,820Earth + Saturn beat frequency

Beat frequency rule

The beat frequencies of consecutive Fibonacci-divided periods satisfy the Fibonacci recurrence:

1H/Fn+1H/Fn+1=FnH+Fn+1H=Fn+2H=1H/Fn+2\frac{1}{H/F_n} + \frac{1}{H/F_{n+1}} = \frac{F_n}{H} + \frac{F_{n+1}}{H} = \frac{F_{n+2}}{H} = \frac{1}{H/F_{n+2}}

This is an algebraic identity, not an empirical fit. For example:

  • 1/111,296+1/66,778=1/41,7361/111{,}296 + 1/66{,}778 = 1/41{,}736 (i.e., 3+5=83 + 5 = 8)
  • 1/66,778+1/41,736=1/25,6841/66{,}778 + 1/41{,}736 = 1/25{,}684 (i.e., 5+8=135 + 8 = 13)
  • 1/41,736+1/25,684=1/15,8991/41{,}736 + 1/25{,}684 = 1/15{,}899 (i.e., 8+13=218 + 13 = 21)

The empirical content of Law 1 is that the precession periods of Earth (H/3H/3), Jupiter (H/5H/5), and Saturn (βˆ’H/8-H/8, retrograde) are related to a single timescale HH through Fibonacci denominators. The higher-order periods (H/13H/13, H/21H/21, H/34H/34) then follow as beat frequencies. See also Precession for the physical meaning of each cycle.

Connection to Laws 2–5: The Fibonacci numbers that organize the timescale hierarchy (3, 5, 8, 13, 21, 34) reappear as the divisors in Laws 2–5. The period denominators bE=3b_E = 3, bJ=5b_J = 5, bS=8b_S = 8 directly determine the ψ\psi-constant via ψ=FbJΓ—FbS2/(FbEΓ—H)\psi = F_{b_J} \times F_{b_S}^2 / (F_{b_E} \times H) β€” see Deriving ψ\psi.


Law 2: Inclination Amplitude

Each planet’s mass-weighted inclination amplitude, multiplied by its Fibonacci divisor, equals the universal ψ\psi-constant:

dΓ—amplitudeΓ—m=ψd \times \text{amplitude} \times \sqrt{m} = \psi

Equivalently:

amplitude=ψdΓ—m\text{amplitude} = \frac{\psi}{d \times \sqrt{m}}

This holds for all 8 planets with a single universal ψ=3.302Γ—10βˆ’3\psi = 3.302 \times 10^{-3}.

Predictions and Laplace-Lagrange validation

PlanetddPredicted amp (Β°)Mean ii (Β°)Range (Β°)LL bounds (Β°)
Mercury210.3866.7286.34 – 7.114.57 – 9.86
Venus340.0622.2082.15 – 2.270.00 – 3.38
Earth30.6351.4810.85 – 2.120.00 – 2.95
Mars51.1632.6531.49 – 3.820.00 – 5.84
Jupiter50.0210.3290.31 – 0.350.24 – 0.49
Saturn30.0650.9320.87 – 1.000.797 – 1.02
Uranus210.0241.0010.98 – 1.020.90 – 1.11
Neptune340.0140.7220.71 – 0.740.55 – 0.80

The equation dΓ—ampΓ—m=ψd \times \text{amp} \times \sqrt{m} = \psi holds by construction. The non-trivial test is that every predicted range (mean Β±\pm amplitude) falls within the Laplace-Lagrange secular theory bounds β€” and all 8 do.

Worked example: Earth’s inclination amplitude

Earth has Fibonacci divisor d=3d = 3 (=F4= F_4). Step by step:

QuantityExpressionValue
ψ\psiF5Γ—F82/(2H)=5Γ—212/667,776F_5 \times F_8^2 / (2H) = 5 \times 21^2 / 667{,}7762205/667,776=3.302005Γ—10βˆ’32205 / 667{,}776 = 3.302005 \times 10^{-3}
ddF4F_43
mmEarth mass (Holistic chain)3.0035Γ—10βˆ’6β€…β€ŠMβŠ™3.0035 \times 10^{-6}\;M_\odot
m\sqrt{m}1.7330Γ—10βˆ’31.7330 \times 10^{-3}
dΓ—md \times \sqrt{m}3Γ—1.7330Γ—10βˆ’33 \times 1.7330 \times 10^{-3}5.1991Γ—10βˆ’35.1991 \times 10^{-3}
amplitude3.302005Γ—10βˆ’3/5.1991Γ—10βˆ’33.302005 \times 10^{-3} / 5.1991 \times 10^{-3}0.635105Β°0.635105Β°

The mean is computed from the J2000 constraint:

mean=iJ2000βˆ’amplitudeΓ—cos⁑(Ξ©J2000βˆ’Ο•group)=1.57867Β°βˆ’0.635105°×cos⁑(284.51Β°βˆ’203.3195Β°)=1.48140Β°\text{mean} = i_\text{J2000} - \text{amplitude} \times \cos(\Omega_\text{J2000} - \phi_\text{group}) = 1.57867Β° - 0.635105Β° \times \cos(284.51Β° - 203.3195Β°) = 1.48140Β°

Fibonacci vs IAU 2006-optimized values

The 3D simulation uses a slightly different value optimized for the IAU 2006 obliquity rate:

ParameterFibonacci predictionIAU 2006 optimizedDifference
Amplitude0.635105Β°0.633849Β°0.001256Β° (4.5β€³)
Mean1.481404Β°1.481596Β°0.000192Β° (0.7β€³)

The 0.20% difference is within the model’s tolerance. The Fibonacci prediction represents the theoretical long-term value from the balance condition, while the IAU 2006-optimized value is calibrated to the currently observed obliquity rate.


Law 3: Inclination Balance

The angular-momentum-weighted inclination amplitudes cancel between the two phase groups, conserving the orientation of the invariable plane:

βˆ‘203° groupLjΓ—ampj=βˆ‘23° groupLjΓ—ampj\sum_{\text{203Β° group}} L_j \times \text{amp}_j = \sum_{\text{23Β° group}} L_j \times \text{amp}_j

Physical motivation

The invariable plane is the fundamental reference plane of the solar system, perpendicular to the total angular momentum vector. For this plane to remain stable, the angular-momentum-weighted inclination oscillations must cancel between the two phase groups. If they didn’t, the total angular momentum vector would wobble β€” violating conservation of angular momentum.

Substituting the Fibonacci formula

With ampj=ψ/(djΓ—mj)\text{amp}_j = \psi / (d_j \times \sqrt{m_j}) and Lj=mjaj(1βˆ’ej2)L_j = m_j \sqrt{a_j(1 - e_j^2)}:

LjΓ—ampj=ΟˆΓ—mjΓ—aj(1βˆ’ej2)dj=ΟˆΓ—wjL_j \times \text{amp}_j = \psi \times \frac{\sqrt{m_j \times a_j(1 - e_j^2)}}{d_j} = \psi \times w_j

Since ψ\psi is a single universal constant, it cancels from both sides:

βˆ‘203Β°wj=βˆ‘23Β°wj\sum_{\text{203Β°}} w_j = \sum_{\text{23Β°}} w_j

where wj=mjΓ—aj(1βˆ’ej2)/djw_j = \sqrt{m_j \times a_j(1 - e_j^2)} / d_j is the structural weight for each planet.

Structural weights

PlanetGroupddwjw_j
Mercury203Β°211.181Γ—10βˆ’51.181 \times 10^{-5}
Venus203Β°343.914Γ—10βˆ’53.914 \times 10^{-5}
Earth203Β°35.776Γ—10βˆ’45.776 \times 10^{-4}
Mars203Β°51.396Γ—10βˆ’41.396 \times 10^{-4}
Jupiter203Β°51.408Γ—10βˆ’21.408 \times 10^{-2}
Uranus203Β°211.375Γ—10βˆ’31.375 \times 10^{-3}
Neptune203Β°341.155Γ—10βˆ’31.155 \times 10^{-3}
Saturn23Β°31.737Γ—10βˆ’21.737 \times 10^{-2}
βˆ‘203Β°w=1.7374Γ—10βˆ’2,βˆ‘23Β°w=1.7374Γ—10βˆ’2\sum_{\text{203Β°}} w = 1.7374 \times 10^{-2}, \quad \sum_{\text{23Β°}} w = 1.7374 \times 10^{-2} Difference:Β 5.4Γ—10βˆ’8,Balance:Β 99.9998%\text{Difference: } 5.4 \times 10^{-8}, \quad \textbf{Balance: 99.9998\%}

Jupiter (d=5d = 5) contributes the dominant 203Β° weight (1.408Γ—10βˆ’21.408 \times 10^{-2}). Saturn (d=3d = 3) alone carries the entire 23Β° contribution. The remaining six 203Β° planets collectively contribute 3.29Γ—10βˆ’33.29 \times 10^{-3} to match the Saturn–Jupiter difference.

TNO contribution

The balance considers only the 8 major planets, which carry 99.994% of the solar system’s orbital angular momentum. Trans-Neptunian Objects (TNOs) contribute the remaining ~0.006%, tilting the invariable plane by approximately 1.25β€³ (Li, Xia & Zhou 2019Β ). The 0.0002% residual imbalance is well within this TNO margin.


Law 4: The Eccentricity Constant

Within each mirror pair, the ratio of eccentricity to mean inclination satisfies two Fibonacci constraints that together determine all eight eccentricities from the inclinations alone.

For each planet, RR measures how it partitions its orbital deviation between eccentricity and inclination. Within each mirror pair, RR values satisfy two Fibonacci constraints β€” an R2R^2 sum and a product or ratio β€” providing two equations for two unknowns.

AMD partition ratio structure

Using J2000 inclinations:

Mirror pairRA2+RB2R^2_A + R^2_BFibonacci ratioError
Mercury / Uranus10.85655/5=1155/5 = 111.33%
Earth / Saturn11.43234/3=11.3334/3 = 11.330.86%
Venus / Neptune0.4801/2=0.51/2 = 0.54.08%
Mars / Jupiter84.905894.82%

Using mean inclinations (more stable than J2000 snapshot):

Mirror pairRA2+RB2R^2_A + R^2_BFibonacci ratioError
Mercury / Uranus10.38921/2=10.521/2 = 10.51.07%
Earth / Saturn11.32234/3=11.3334/3 = 11.330.10%
Venus / Neptune0.4961/2=0.51/2 = 0.50.91%
Mars / Jupiter75.020377/5=75.4377/5 = 75.40.51%

This connects to AMD theory (Laskar 1997): Ckβ‰ˆΞ›k(e2/2+i2/2)C_k \approx \Lambda_k(e^2/2 + i^2/2) for small ee and ii. The ratio R2+1=(e2+i2)/i2R^2 + 1 = (e^2 + i^2)/i^2 determines how each planet partitions its angular momentum deficit between eccentricity and inclination.

Fibonacci pair constraints

The pair sums alone provide one equation for two unknowns. Crucially, pair products and ratios are also Fibonacci, providing a second equation that determines individual eccentricities:

Mirror pairConstraint 1FibonacciConstraint 2Fibonacci
Mercury / UranusRMe2+RUr2R^2_\text{Me} + R^2_\text{Ur}21/2=10.521/2 = 10.5RMe/RUrR_\text{Me} / R_\text{Ur}2/32/3
Venus / NeptuneRVe2+RNe2R^2_\text{Ve} + R^2_\text{Ne}1/2=0.51/2 = 0.5RVe/RNeR_\text{Ve} / R_\text{Ne}2/8=0.252/8 = 0.25
Earth / SaturnREa2+RSa2R^2_\text{Ea} + R^2_\text{Sa}34/3β‰ˆ11.3334/3 \approx 11.33REaΓ—RSaR_\text{Ea} \times R_\text{Sa}22
Mars / JupiterRMa2+RJu2R^2_\text{Ma} + R^2_\text{Ju}377/5=75.4377/5 = 75.4RMaΓ—RJuR_\text{Ma} \times R_\text{Ju}34/2=1734/2 = 17

Belt-adjacent pairs (Mars/Jupiter, Earth/Saturn) use a product constraint; outer pairs (Venus/Neptune, Mercury/Uranus) use a ratio constraint β€” reflecting the different coupling regimes across the asteroid belt.

Dynamical implication β€” communicating vessels: The product constraint REaΓ—RSa=2R_\text{Ea} \times R_\text{Sa} = 2 implies that Earth’s and Saturn’s eccentricities cannot evolve independently. Since R=e/imean,radR = e / i_\text{mean,rad}, a decrease in Earth’s eccentricity (currently heading toward its ∼0.0139{\sim}0.0139 minimum around 11,680 AD) reduces REaR_\text{Ea}, forcing RSaR_\text{Sa} to increase β€” and with it Saturn’s eccentricity. The coupling is bidirectional: Saturn has its own perihelion precession cycle (βˆ’H/8=41,736-H/8 = 41{,}736 years, retrograde), which drives its own eccentricity changes. Through the product constraint, those changes feed back into Earth’s eccentricity. The two planets behave like communicating vessels: what one loses in eccentricity, the other gains, mediated by the Fibonacci product constraint.

An observational clue supports this coupling: Earth’s eccentricity is currently decreasing while Saturn’s is increasing β€” exactly as the product constraint predicts. This bidirectional coupling may explain residual discrepancies between the model’s eccentricity curve and the formula-based predictions for Earth: the current model computes Earth’s eccentricity from its own 20,868-year perihelion cycle alone, without accounting for the additional perturbation from Saturn’s eccentricity evolution feeding back through the pair constraint. The physical coupling is already present in the precession formulas: Saturn is the only planet whose precession formula requires Earth’s time-varying obliquity and eccentricity as inputs (GROUP 15 terms; see Formulas).

Quantifying the coupling. If REaΓ—RSa=2R_\text{Ea} \times R_\text{Sa} = 2 holds as a dynamical invariant and the mean inclinations are constant, then the product of eccentricities is fixed:

eE(t)Γ—eSa(t)=2Γ—iE,radΓ—iSa,rad=2Γ—0.025862Γ—0.016262β‰ˆ0.00084e_E(t) \times e_{Sa}(t) = 2 \times i_{E,\text{rad}} \times i_{Sa,\text{rad}} = 2 \times 0.025862 \times 0.016262 \approx 0.00084

Using the model’s eccentricity range for Earth (0.01390.0139–0.01670.0167), the constraint predicts Saturn’s eccentricity range:

Earth eeRER_ERSa=2/RER_{Sa} = 2/R_ESaturn ee
0.0167 (max)0.6463.0970.0504
0.0153 (base)0.5923.3780.0549
0.0139 (min)0.5383.7210.0605

Conversely, Saturn’s own H/8=41,736H/8 = 41{,}736-year perihelion cycle feeds back into Earth with an amplitude of ∼±0.0015\sim\pm 0.0015 β€” comparable to Earth’s own eccentricity amplitude (0.0014). The combined effect distorts the eccentricity curve from a pure sinusoid, potentially shifting the minimum depth and timing by several thousand years.

Impact on derived quantities. Through the regression formula Ysid(days)=f(e)Y_\text{sid}(\text{days}) = f(e) (with coefficient k2=3,208k_2 = 3{,}208 s/unit eccentricity), Saturn’s Β±0.0015\pm 0.0015 modulation translates to a Length of Day variation of ∼±0.1\sim\pm 0.1 ms β€” detectable but modest compared to the Β±4\pm 4–55 ms total variation from Earth’s own cycle. The sidereal year in seconds is unaffected: it depends on Earth’s semi-major axis (Kepler’s third law), not on eccentricity, and secular perturbations preserve semi-major axes to first order.

Comparison with secular theory. Conventional Laplace-Lagrange theory gives Saturn’s dominant eccentricity eigenfrequency (g6=28.245g_6 = 28.245β€œ/yr) a period of ∼46,000\sim 46{,}000 years β€” intriguingly close to H/8=41,736H/8 = 41{,}736 years. Whether these represent the same physical period is testable. Note that the connection between Earth and Saturn is purely orbital: Saturn’s axial (spin-axis) precession has a period of ∼1.8\sim 1.8 Myr, driven by a spin-orbit resonance with Neptune’s nodal mode s8s_8 (Saillenfest et al. 2021), and is unrelated to the Fibonacci timescale hierarchy.

Whether REaΓ—RSa=2R_\text{Ea} \times R_\text{Sa} = 2 holds as a dynamical invariant over the full perihelion cycle is a testable prediction of the model β€” as is the question of whether the same communicating-vessel behaviour holds for the other three mirror pairs (Mars/Jupiter, Venus/Neptune, Mercury/Uranus).

Predictions β€” zero free parameters

Solving each pair gives predicted RR values, and thus predicted eccentricities via epred=RpredΓ—imean,rade_\text{pred} = R_\text{pred} \times i_\text{mean,rad}:

Planetee predictedee actual (JPL)Error
Mercury0.211060.20563+2.64%
Venus0.006610.00678βˆ’2.50%-2.50\%
Earth0.015620.01533+1.92%
Mars0.093200.09340βˆ’0.21%-0.21\%
Jupiter0.048520.04839+0.28%
Saturn0.053890.05386+0.05%+0.05\%
Uranus0.047090.04726βˆ’0.36%-0.36\%
Neptune0.008650.00859+0.65%

Total |error|: 8.57%. Eccentricity balance (Law 5) cross-check: 99.93%.

Mars/Jupiter achieves extraordinary precision (0.49% pair error), and Saturn is predicted to within 0.05%. The inner pairs (Mercury/Uranus, Venus/Neptune) show 2–3% errors per planet, which trace to the mathematical amplification of the smaller RR value in each pair rather than any systematic inner/outer asymmetry.

This law partially resolves Open Question 1: while no universal closed-form eccentricity formula exists, all eight eccentricities are predicted from inclinations via Fibonacci pair constraints on the AMD partition ratio.


Law 5: Eccentricity Balance

The eccentricities satisfy an independent balance condition using the same Fibonacci divisors and phase groups:

βˆ‘203° groupvj=βˆ‘23° groupvj\sum_{\text{203Β° group}} v_j = \sum_{\text{23Β° group}} v_j

where

vj=mjΓ—aj3/2Γ—ej/djv_j = \sqrt{m_j} \times a_j^{3/2} \times e_j / \sqrt{d_j}

Or equivalently, in terms of orbital period Tj∝aj3/2T_j \propto a_j^{3/2}:

vj=TjΓ—ejΓ—mj/djv_j = T_j \times e_j \times \sqrt{m_j / d_j}

Eccentricity balance weights

PlanetGroupddvj=mΓ—a3/2Γ—e/dv_j = \sqrt{m} \times a^{3/2} \times e / \sqrt{d}
Mercury203Β°214.404Γ—10βˆ’64.404 \times 10^{-6}
Venus203Β°341.119Γ—10βˆ’61.119 \times 10^{-6}
Earth203Β°31.533Γ—10βˆ’51.533 \times 10^{-5}
Mars203Β°54.463Γ—10βˆ’54.463 \times 10^{-5}
Jupiter203Β°57.928Γ—10βˆ’37.928 \times 10^{-3}
Uranus203Β°215.705Γ—10βˆ’35.705 \times 10^{-3}
Neptune203Β°341.734Γ—10βˆ’31.734 \times 10^{-3}
Saturn23Β°31.547Γ—10βˆ’21.547 \times 10^{-2}
βˆ‘203Β°v=1.543Γ—10βˆ’2,βˆ‘23Β°v=1.547Γ—10βˆ’2\sum_{\text{203Β°}} v = 1.543 \times 10^{-2}, \quad \sum_{\text{23Β°}} v = 1.547 \times 10^{-2} Balance:Β 99.88%\textbf{Balance: 99.88\%}

Saturn alone carries the entire 23Β° contribution. The 203Β° group is dominated by Jupiter (7.928Γ—10βˆ’37.928 \times 10^{-3}), Uranus (5.705Γ—10βˆ’35.705 \times 10^{-3}), and Neptune (1.734Γ—10βˆ’31.734 \times 10^{-3}), with the four inner planets contributing only 6.6Γ—10βˆ’56.6 \times 10^{-5} combined.

Comparing the two balance conditions

PropertyInclination weight wjw_jEccentricity weight vjv_j
FormulamΓ—a(1βˆ’e2)/d\sqrt{m \times a(1-e^2)} / dmΓ—a3/2Γ—e/d\sqrt{m} \times a^{3/2} \times e / \sqrt{d}
dd scaling1/d1/d1/d1/\sqrt{d}
aa scalinga\sqrt{a}a3/2a^{3/2}
ee roleWeak (1βˆ’e2β‰ˆ11 - e^2 \approx 1)Direct (linear in ee)

The half-power difference in Fibonacci divisor scaling (1/d1/d vs 1/d1/\sqrt{d}) and the shift from a\sqrt{a} to a3/2a^{3/2} reflect that the eccentricity balance operates at a different order in secular perturbation theory.

The eccentricity balance is not a structural artifact β€” see Finding 3 for three independence tests.

Connection to AMD theory

The established AMD formula of Laskar (1997) couples eccentricity and inclination through a single conserved quantity: Ck=mkΞΌak(1βˆ’1βˆ’ek2cos⁑ik)C_k = m_k \sqrt{\mu a_k}(1 - \sqrt{1-e_k^2}\cos i_k). For small ee and ii: Ckβ‰ˆΞ›k(e2/2+i2/2)C_k \approx \Lambda_k(e^2/2 + i^2/2).

The eccentricity balance operates on linear ee rather than e2e^2, suggesting it captures a first-order secular constraint distinct from the quadratic AMD conservation. The physical mechanism producing this linear balance remains an open question.


Law 6: The Saturn-Jupiter-Earth Resonance

Saturn’s retrograde precession creates a closed beat-frequency loop with Jupiter and Earth β€” the physical mechanism linking the Fibonacci timescale (Law 1) to orbital structure (Laws 2–5).

Saturn is the only planet whose perihelion precesses retrograde (period =βˆ’H/8= -H/8). When its retrograde motion interacts with Jupiter’s prograde motion (H/5H/5), the resulting beat frequencies form a closed loop:

RelationshipCalculationResult
Earth + Jupiter β†’ SaturnF4/H+F5/HF_4/H + F_5/H=F6/H=1/41,736= F_6/H = 1/41{,}736 = Obliquity / Saturn (H/8H/8)
Saturn βˆ’ Jupiter β†’ EarthF6/Hβˆ’F5/HF_6/H - F_5/H=F4/H=1/111,296= F_4/H = 1/111{,}296 = Earth inclination (H/3H/3)
Saturn βˆ’ Earth β†’ JupiterF6/Hβˆ’F4/HF_6/H - F_4/H=F5/H=1/66,778= F_5/H = 1/66{,}778 = Jupiter (H/5H/5)

All three rows are cyclic permutations of 3+5=83 + 5 = 8. Each planet’s period is the beat frequency of the other two:

Saturn (H/8) β•± β•² 8βˆ’5=3 8βˆ’3=5 β•± β•² Earth (H/3) ──3+5=8── Jupiter (H/5)

This also connects to Law 1: combining Jupiter (H/5H/5) and Saturn (H/8H/8) produces axial precession: F5/H+F6/H=F7/H=1/25,684F_5/H + F_6/H = F_7/H = 1/25{,}684 (i.e., 5+8=135 + 8 = 13).

Why this is a Fibonacci identity

The closed loop is an algebraic consequence of the Fibonacci addition rule applied to the period denominators:

bE+bJ=bS⇒3+5=8b_E + b_J = b_S \quad \Rightarrow \quad 3 + 5 = 8

Since Fn/H+Fn+1/H=Fn+2/HF_n/H + F_{n+1}/H = F_{n+2}/H, the beat frequency rule is just the Fibonacci recurrence in disguise. The empirical content is that Earth, Jupiter, and Saturn have period denominators bE=3b_E = 3, bJ=5b_J = 5, bS=8b_S = 8 β€” three consecutive Fibonacci numbers with Saturn as the sum.

Connection to the ψ-constant

The same three planets and their period denominators determine the inclination constant:

ψ=FbJΓ—FbS2FbEΓ—H=F5Γ—F82F3Γ—H\psi = \frac{F_{b_J} \times F_{b_S}^2}{F_{b_E} \times H} = \frac{F_5 \times F_8^2}{F_3 \times H}

Law 6 thus reveals why Earth, Jupiter, and Saturn hold special roles throughout the Fibonacci Laws: they are the three planets locked into a Fibonacci resonance triangle, and their period denominators drive both the timescale hierarchy (Law 1) and the inclination constant (Law 2).

Physical interpretation: Saturn’s retrograde precession is the fulcrum that converts Fibonacci arithmetic into physical reality. Each of the three planets β€” Earth, Jupiter, Saturn β€” has a precession period equal to the beat frequency of the other two (3+5=83 + 5 = 8). Combining Jupiter and Saturn further produces axial precession (5+8=135 + 8 = 13). The same three planets dominate the inclination balance (Law 3) and the eccentricity balance (Law 5).


Findings

Findings are empirical observations and consequences that follow from the six laws.

Finding 1: Mirror Symmetry

As shown in the Planet Configuration table, each inner planet shares its dd with its outer counterpart across the asteroid belt: Mars ↔ Jupiter (F5F_5), Earth ↔ Saturn (F4F_4), Venus ↔ Neptune (F9F_9), Mercury ↔ Uranus (F8F_8). Earth–Saturn is the only pair with opposite phase groups (203Β° vs 23Β°). The divisors form two consecutive Fibonacci pairs: (3,5)(3, 5) for the belt-adjacent planets and (21,34)(21, 34) for the outer planets.

Finding 2: Configuration Uniqueness

The exhaustive search tested 7,558,272 configurations against four independent physical constraints:

FilterPassingPercentage
Inclination balance β‰₯ 99.994%7550.010%
Mirror-symmetric assignments2,5920.034%
Saturn as sole retrograde planet236,1963.1%
Laplace-Lagrange bounds compliance739,2009.8%

Each filter independently eliminates most of the search space. The most restrictive three-filter intersection (Saturn-solo + balance + Laplace-Lagrange) yields only 7 configurations. Adding mirror symmetry leaves exactly one: Config #32 (0.0000132% of the search space).

Since Earth is locked at d=3d = 3, only Scenario A (Saturn d=3d = 3) can satisfy the Earth↔Saturn mirror symmetry. No other planet configuration produces the required mirror pairing while simultaneously satisfying all physical constraints.

The search space covers:

  • Fibonacci divisors: d∈{1,2,3,5,8,13,21,34,55}d \in \{1, 2, 3, 5, 8, 13, 21, 34, 55\} for Mercury, Venus, Mars, Uranus, Neptune
  • Phase angles: 203.3195Β° or 23.3195Β° for each of the above
  • 4 scenarios for Jupiter and Saturn (fixed per scenario): A: Ju=5, Sa=3 β€” B: Ju=8, Sa=5 β€” C: Ju=13, Sa=8 β€” D: Ju=21, Sa=13
  • Earth: locked at d=3d = 3, phase = 203.3195Β°
  • Total: 9Γ—2Γ—9Γ—2Γ—9Γ—2Γ—9Γ—2Γ—9Γ—2Γ—4=7,558,2729 \times 2 \times 9 \times 2 \times 9 \times 2 \times 9 \times 2 \times 9 \times 2 \times 4 = 7{,}558{,}272 configurations

The mirror symmetry was not assumed β€” it emerged from the exhaustive search as the unique configuration satisfying all constraints simultaneously: (1) all planets within Laplace-Lagrange bounds, (2) inclination balance >99.994%> 99.994\%, and (3) eccentricity balance >99.5%> 99.5\%.

Finding 3: Eccentricity Balance Independence

The eccentricity balance (Law 5) is genuinely independent from the inclination balance (Law 3). Three tests confirm it is not a structural artifact:

  1. Coefficient test: The weight formula without eccentricities (mΓ—a3/2/d\sqrt{m} \times a^{3/2} / \sqrt{d}) gives only 74% balance β€” the actual eccentricity values contribute 26 percentage points of improvement
  2. Random test: Substituting random eccentricities into the same weight formula gives 50–85% balance across 1,000 trials
  3. Power test: The balance peaks sharply at e1.0e^{1.0} (99.88%), dropping to 98.5% for e0.9e^{0.9} and 98.4% for e1.1e^{1.1}, and to 91% for e2e^2 β€” linear eccentricity is special

Additionally, the ratio vj/wjv_j/w_j varies by a factor of ~150 across planets, confirming the two balance conditions are not proportional.

Finding 4: Saturn Eccentricity Prediction and Law Convergence

Since Saturn is the sole retrograde planet, the eccentricity balance directly predicts its eccentricity from the other seven:

eSaturn=βˆ‘203° groupvjmSaΓ—aSa3/2/dSae_\text{Saturn} = \frac{\sum_{\text{203Β° group}} v_j}{\sqrt{m_\text{Sa}} \times a_\text{Sa}^{3/2} / \sqrt{d_\text{Sa}}}

Two structurally independent laws predict Saturn’s eccentricity β€” and bracket the observed value:

SourceeSaturne_\text{Saturn}vs J2000
Law 4 (RΒ² pair constraint)0.05389+0.05%+0.05\%
Law 5 (eccentricity balance)0.05373βˆ’0.24%-0.24\%
J2000 observed (JPL DE440)0.05386β€”

Law convergence: Laws 4 and 5 independently predict Saturn’s eccentricity to within 0.30% of each other. Law 4 derives it from the R2R^2 pair constraint (RE2+RSa2=34/3R^2_E + R^2_{Sa} = 34/3) β€” a purely structural Fibonacci relation using only the Earth-Saturn pair. Law 5 derives it from the global balance equation involving all eight planets simultaneously. Both bracket the J2000 observed value: Law 4 overshoots by 0.05%, Law 5 undershoots by 0.24%.

Why this is significant: Saturn’s eccentricity oscillates secularly between ~0.01 and ~0.09 (a factor-of-9 dynamic range). Two structurally different Fibonacci constraints β€” one using only the Earth-Saturn pair, the other using all eight planets β€” independently predict a value within 0.3% of each other and within 0.25% of J2000 across this range. The Fibonacci divisors were originally chosen to match precession periods (Law 1) and inclination balance (Law 3); the eccentricity predictions were never optimized for.

Overconstrained system: The 8 pair constraints (Law 4) plus Law 5 provide 9 equations for 8 unknowns (the eccentricities). The system is overconstrained by one equation β€” Saturn’s eccentricity is predicted by both laws independently. That two equations drawing on different subsets of planetary data converge on the same value confirms that the eccentricity balance is not an independent free parameter but an emergent consequence of the Fibonacci pair structure.

The 0.12% gap between the observed balance (99.88%) and perfect balance traces directly to Saturn’s J2000 eccentricity (0.05386) being 0.24% above the Law 5 equilibrium prediction (0.05373). The Law 5 prediction represents the eccentricity at which the balance would be exact.

Finding 5: Inner Planet Eccentricity Ladder

The mass-weighted eccentricities of the four inner planets form a Fibonacci ratio sequence:

ΞΎV:ΞΎE:ΞΎMars:ΞΎMercury=1:5/2:5:8\xi_V : \xi_E : \xi_\text{Mars} : \xi_\text{Mercury} = 1 : 5/2 : 5 : 8

where ΞΎ=eΓ—m\xi = e \times \sqrt{m}. Consecutive ratios are 5/25/2, 22, 8/58/5 β€” all converging toward the golden ratio Ο†β‰ˆ1.618\varphi \approx 1.618.

Earth’s base eccentricity (0.015321), independently determined from the 3D simulation, anchors the ladder at position 5/25/2:

PlanetFib. mult.ee predictedee actualError
Venus10.006790.00678 (J2000)+0.16%
Earth5/20.015320.01532 (base)reference
Mars50.093470.09339 (J2000)+0.09%
Mercury80.208530.20564 (J2000)+1.41%

Venus cross-validation: The ladder predicts eV=0.006788e_V = 0.006788 from Earth’s independently determined base eccentricity. This matches the measured J2000 value (0.006777) to 0.16% β€” confirming the ladder from a completely independent direction.

Finding 6: No Universal Eccentricity Constant

A comprehensive search across ~30 physical and Fibonacci parameters confirms that no combination ΞΎΓ—f(observables)\xi \times f(\text{observables}) yields a planet-universal constant analogous to the inclination ψ\psi.

The search tested all power-law combinations of: semi-major axis, orbital period, mass, inclination precession period, perihelion precession period, AMD, Hill radius, orbital angular momentum, secular eigenfrequencies (gg- and ss-modes), Kozai integral, mean inclination, eccentricity half-angle h(e)h(e), Fibonacci divisors (dd, bb), and cross-parameter ratios β€” across 1-, 2-, 3-, and 4-parameter combinations with fractional exponents.

Results (excluding tautologies that restate the inclination law):

Best spreadFormulaInterpretation
0.54%ΞΎ/f(e)β‹…m\xi / \sqrt{f(e) \cdot m}Reduces to h(e)=e/1βˆ’1βˆ’e2β‰ˆ2h(e) = e/\sqrt{1-\sqrt{1-e^2}} \approx \sqrt{2} β€” a mathematical identity for small ee with no discriminating power
23%ΞΎ/Ξ£β‹…m\xi / \sqrt{\Sigma \cdot m} where Ξ£=e2+i2\Sigma = e^2 + i^2Best genuine physics combination; Earth is a 19% outlier
195%ΞΎ/AMD\xi / \sqrt{\text{AMD}}Best single-parameter result; proven to be an identity 2/a\sqrt{2/\sqrt{a}} where eccentricity cancels

The fundamental reason: the inclination divisors dd span only 11Γ— (from 3 to 34), allowing a single ψ\psi to work. The eccentricity multipliers kk span 141Γ— (from 1 to 141) with no smooth dependence on any present-day observable. The eccentricity ladder is a formation constraint imprinted during the dissipative epoch, not derivable from current orbital mechanics.

Script: fibonacci_eccentricity_constant.py β€” modular search engine with ~30 parameters, 9 search strategies, and fine-grid refinement.


Deriving ψ\psi from the Holistic Year

The inclination constant ψ\psi was initially a calibration parameter β€” measured from the data but not derived from first principles. A systematic search reveals it can be expressed exactly in terms of HH and Fibonacci numbers:

ψ=F5Γ—F822H=5Γ—212667,776=2205667,776\psi = \frac{F_5 \times F_8^2}{2H} = \frac{5 \times 21^2}{667{,}776} = \frac{2205}{667{,}776}

This predicts ψ=3.302005Γ—10βˆ’3\psi = 3.302005 \times 10^{-3}. Combined with the Fibonacci divisors and the balance condition, this single value determines all eight inclination amplitudes β€” and every predicted range falls within the Laplace-Lagrange secular theory bounds.

Physical interpretation: the E–J–S period connection

The Fibonacci indices 5 and 8 are the period denominators of Jupiter and Saturn (from Law 1: H/5H/5 and H/8H/8). The denominator factor 2 = F3=FbEF_3 = F_{b_E} is Earth’s contribution:

ψ=FbJΓ—FbS2FbEΓ—H\psi = \frac{F_{b_J} \times F_{b_S}^2}{F_{b_E} \times H}

where bE=3b_E = 3, bJ=5b_J = 5, bS=8b_S = 8 are the period denominators of Earth, Jupiter, and Saturn, satisfying the Fibonacci addition 3+5=83 + 5 = 8.

PlanetPeriod denominator bbFbF_bRole in ψ\psi
Earth3F3=2F_3 = 2denominator
Jupiter5F5=5F_5 = 5numerator
Saturn8F8=21F_8 = 21numerator (squared)

Saturn’s FbF_b appears squared, reflecting its special role as the β€œsum planet” (bS=bE+bJb_S = b_E + b_J). These same three planets dominate the inclination balance condition β€” Jupiter and Saturn are the dominant contributors to the 203Β° and 23Β° phase groups respectively.

Equivalently, ΟˆΓ—TV/N=F5Γ—F82=2205\psi \times T_{V/N} = F_5 \times F_8^2 = 2205, where TV/N=2HT_{V/N} = 2H is the period shared by Venus and Neptune. This connects the amplitude structure (how much planets tilt) to the period structure (how fast they oscillate).

Complete prediction chain: Given only H=333,888H = 333{,}888, a planet’s mass, and its Fibonacci divisor dd, the inclination amplitude is fully determined. No observed orbital elements are needed as input.


The Master Ratio Rβ‰ˆ311R \approx 311

Since ψ\psi is fixed by HH and Fibonacci numbers, the eccentricity scale is determined by a single ratio:

R=ψξV=2205/(2H)eVΓ—mVβ‰ˆ311R = \frac{\psi}{\xi_V} = \frac{2205 / (2H)}{e_V \times \sqrt{m_V}} \approx 311

Since 311 is prime and not expressible as a Fibonacci product, the two structures remain connected but not unified. The eccentricity base unit ΞΎV\xi_V requires one independent measurement β€” Earth’s base eccentricity eE=0.015321e_E = 0.015321 from the 3D simulation.

However, 311 is not an arbitrary prime β€” it is a Fibonacci primitive root prime (OEIS A003147Β ): the Fibonacci sequence mod 311 has the maximal possible period Ο€(311)=310=pβˆ’1\pi(311) = 310 = p - 1, visiting every non-zero residue class before repeating. Only ~27% of primes have this property.

Two-layer explanation:

  1. Why an FPR prime? In a system where coupling strengths decay as powers of Ο†\varphi (as the Fibonacci quantum numbers require), an FPR prime ensures maximal compatibility β€” no β€œdead zones” in the coupling spectrum. Additionally, Ξ±(311)=310=Ο€(311)\alpha(311) = 310 = \pi(311) (Type 1, maximally efficient entry point).

  2. Why 311 specifically? Among the 33 FPR primes ≀600\leq 600, 311 is the closest to the formation-epoch value R=310.83R = 310.83 (distance 0.17; next-nearest are 271 at distance 40 and 359 at distance 48). The fractional part Rβ‰ˆ311βˆ’F3/F7=311βˆ’2/13R \approx 311 - F_3/F_7 = 311 - 2/13 at 0.007%.

The same number 311 appears as the optimal super-period in the TRAPPIST-1 system β€” see Exoplanet Tests.

The eccentricity ladder is a formation constraint (p<10βˆ’5p < 10^{-5} from Monte Carlo), not dynamically selected. This explains why RR cannot be derived from HH β€” the eccentricity scale was set by initial conditions during the dissipative formation epoch, making one free parameter (eEe_E, or equivalently Rβ‰ˆ311R \approx 311) irreducible.


Physical Foundations

Why m\sqrt{m}: the Angular Momentum Deficit connection

The quantity ΞΎ=eΓ—m\xi = e \times \sqrt{m} (or Ξ·=iΓ—m\eta = i \times \sqrt{m}) has a direct connection to the Angular Momentum Deficit (AMD), the standard dynamical quantity in celestial mechanics:

AMDiβ‰ˆai2(ΞΎi2+Ξ·i2)\text{AMD}_i \approx \frac{\sqrt{a_i}}{2} \left( \xi_i^2 + \eta_i^2 \right)

where ΞΎi=eimi\xi_i = e_i \sqrt{m_i} and Ξ·i=iimi\eta_i = i_i \sqrt{m_i} are exactly the mass-weighted quantities used in the Fibonacci laws. The m\sqrt{m} exponent is uniquely determined by the AMD decomposition β€” no other mass power produces this sum-of-squares form.

Empirical confirmation: Testing the ψ\psi-constant (dΓ—iΓ—mΞ±d \times i \times m^\alpha) across Venus, Earth, and Neptune for different mass exponents:

Ξ±\alphaSpread across 3 planets
0.2542%
0.3330%
0.500.11%
0.6735%
1.00106%

The exponent Ξ±=0.50\alpha = 0.50 is optimal by a factor of ∼250Γ—\sim 250\times over the next-best alternative.

Connection to KAM theory

The appearance of Fibonacci numbers in mass-weighted orbital parameters has a theoretical explanation through KAM (Kolmogorov-Arnold-Moser) theory:

  1. KAM theorem (Kolmogorov 1954, Arnold 1963, Moser 1962): Orbits survive if their frequency ratio satisfies a Diophantine condition β€” a quantitative measure of irrationality.

  2. Golden ratio optimality (Hurwitz 1891): The golden ratio Ο†=[1;1,1,1,…]\varphi = [1; 1, 1, 1, \ldots] has the slowest-converging continued fraction, making it the hardest irrational number to approximate by rationals. Fibonacci ratios Fn+1/FnF_{n+1}/F_n are its convergents.

  3. Greene-Mackay criterion (Greene 1979): The last invariant torus to break as perturbation increases has frequency ratio equal to Ο†\varphi. Morbidelli & Giorgilli (1995) proved golden-ratio KAM tori have superexponentially long stability times.

  4. Natural selection over 4.6 Gyr: Orbits near low-order rational resonances are disrupted (Kirkwood gaps). Orbits near golden-ratio KAM tori survive. The surviving population is organized around Fibonacci ratios.

  5. AMD variables: The quantities ΞΎ=em\xi = e\sqrt{m} and Ξ·=im\eta = i\sqrt{m} are the natural action-like variables in the secular Hamiltonian. KAM stability conditions constrain these to Fibonacci ratios.

This chain β€” KAM stability β†’ Diophantine condition β†’ golden ratio β†’ Fibonacci convergents β†’ Fibonacci structure in ΞΎ\xi and Ξ·\eta β€” provides the theoretical foundation for why Fibonacci numbers specifically appear.

Time independence

The Fibonacci laws use oscillation amplitudes (secular eigenmode properties), not instantaneous orbital elements. The ψ\psi-constants and balance conditions use amplitudes Ξ·=iampΓ—m\eta = i_\text{amp} \times \sqrt{m} β€” properties of secular eigenmodes that are exactly time-independent by construction. The eccentricity ladder acts on base eccentricities that encode a formation-epoch constraint, preserved in the eigenmodes since the dissipative era.


Statistical Significance

Molchanov’s 1968 work was criticized by Backus (1969) for not proving statistical significance. To address this, a comprehensive significance analysis was performed using three independent null models and twelve test statistics covering all six laws, explicitly accounting for the look-elsewhere effect.

Methodology. Twelve test statistics were computed for the real Solar System and compared against random planetary systems:

  1. Pairwise Fibonacci count β€” How many of the 56 pairwise ΞΎ\xi-ratios and Ξ·\eta-ratios match Fibonacci ratios within 5%? Observed: 21/56.
  2. Eccentricity ladder (Finding 5) β€” For the best 4-planet subset, how many ΞΎ\xi-ratios match Fibonacci ratios within 3%? Observed: 3 matches (mean error 0.49%).
  3. ψ\psi-constant (3-planet) β€” How small is the relative spread of dΓ—iΓ—md \times i \times \sqrt{m} for the best 3-planet subset with Fibonacci weights? Observed: 16.97%.
  4. Cross-parameter ratio β€” Does (Ξ›ecc+Ξ›amp)/Ξ›mean(\Lambda_\text{ecc} + \Lambda_\text{amp}) / \Lambda_\text{mean} match an extended Fibonacci ratio? Observed: 5.43% error.
  5. Inclination balance (Law 3) β€” With the model’s Fibonacci dd-values and phase groups, how well do the structural weights wjw_j cancel? Observed: 99.9998%.
  6. Eccentricity balance (Law 5) β€” With the same dd-values and phase groups, how well do the eccentricity weights vjv_j cancel? Observed: 99.88%.
  7. Saturn eccentricity prediction (Finding 4) β€” Law 4 and Law 5 independently predict Saturn’s ee: 0.05389 (+0.05%) and 0.05373 (βˆ’0.24%), bracketing J2000. Law convergence: 0.30%.
  8. ψ\psi-constant, full 8-planet (Law 2) β€” How small is the spread of dΓ—iJ2000Γ—md \times i_\text{J2000} \times \sqrt{m} across all 8 planets using J2000 inclinations? Observed: 234.7% spread.
  9. Precession hierarchy (Law 1) β€” How many pairwise ratios of precession periods H/FnH/F_n match Fibonacci ratios? Observed: 10 pairs.
  10. R2R^2 partition (Law 4) β€” For each mirror pair, does Rinner2+Router2R_\text{inner}^2 + R_\text{outer}^2 (where R=e/iradR = e/i_\text{rad}) match a Fibonacci ratio? Observed: 4/4 pairs match.
  11. E–J–S resonance (Law 6) β€” Do the period denominators satisfy bE+bJ=bSb_E + b_J = b_S? Observed: exact (3+5=83 + 5 = 8).
  12. Mirror symmetry (Finding 1) β€” How many of the 4 inner–outer mirror pairs share the same dd-value? Observed: 4/4 pairs match.

Circularity note: Tests 3–4 use inclination amplitudes derived from the Fibonacci formula (amp=ψ/(dΓ—m)\text{amp} = \psi / (d \times \sqrt{m})), making their observed values artificially tight. The permutation test is still valid (shuffling masses breaks the structure), but the observed statistics are circular. Test 8 avoids this by using J2000 inclinations instead. All other tests are fully independent of the model’s derived quantities.

Tests 5–7 use the model’s fixed Fibonacci dd-assignments and phase groups β€” zero look-elsewhere effect. Tests 1–4 involve implicit optimization (searching over subsets, weight assignments, or Fibonacci ratios), but this is accounted for automatically because each random trial computes the same optimized statistics. Tests 10–12 depend on planet identity (mirror-pair assignments, period fractions, and dd-assignments), making them insensitive to the permutation test but testable via Monte Carlo.

Three null distributions were tested:

  • Permutation (exhaustive, 8!=40,3208! = 40{,}320 trials): same eccentricity and amplitude values, randomly reassigned to planets. For Tests 5–7: model dd-values are kept, eccentricities are shuffled among planets. Tests 11–12 are identity-dependent and always match in this null (p=1p = 1).
  • Log-uniform Monte Carlo (100,000100{,}000 trials): random eccentricities from [0.005,0.25][0.005, 0.25], amplitudes from [0.01Β°,3.0Β°][0.01Β°, 3.0Β°], means from [0.1Β°,10Β°][0.1Β°, 10Β°] (log-uniform). Random dd-values from {1,2,3,5,8,13,21,34,55}\{1, 2, 3, 5, 8, 13, 21, 34, 55\}, random precession periods, random period fractions from {1,2,3,5,8,13,21,34}\{1, 2, 3, 5, 8, 13, 21, 34\}.
  • Uniform Monte Carlo (100,000100{,}000 trials): same ranges, flat distribution. Same null model for Tests 5–12.

Masses are fixed at solar system values throughout (conservative).

Results (permutation: exhaustive 8!8!; Monte Carlo: 100,000100{,}000 trials):

TestObservedPermutationLog-uniformUniform
1. Pairwise count21/56p=0.018p = 0.018p=0.009p = 0.009p=0.014p = 0.014
2. Ecc. ladder3 matchesp=0.35p = 0.35p=0.37p = 0.37p=0.40p = 0.40
3. ψ\psi-constant16.97%p=0.82p = 0.82p=0.86p = 0.86p=0.94p = 0.94
4. Cross-parameter5.43%p=0.58p = 0.58p=0.49p = 0.49p=0.48p = 0.48
5. Incl. balance99.9998%p=0.00057p = 0.00057p<10βˆ’5p < 10^{-5}p<10βˆ’5p < 10^{-5}
6. Ecc. balance99.88%p=0.00067p = 0.00067p=0.0003p = 0.0003p=0.0005p = 0.0005
7. Saturn pred.0.24%p=0.00067p = 0.00067p=0.0003p = 0.0003p=0.0005p = 0.0005
8. ψ\psi full234.7%p=0.047p = 0.047p=0.017p = 0.017p=0.027p = 0.027
9. Prec. hierarchy10 pairsp=0.83p = 0.83p=0.91p = 0.91p=0.79p = 0.79
10. R2R^2 partition4/4p=0.32p = 0.32 ‑p=0.0009p = 0.0009p=0.027p = 0.027
11. E–J–S reson.exactp=1p = 1 ‑p=0.033p = 0.033p=0.032p = 0.032
12. Mirror symm.4/4p=1p = 1 ‑p=0.0002p = 0.0002p=0.0002p = 0.0002
Fisher’s combinedp=1.4Γ—10βˆ’5p = 1.4 \times 10^{-5}p=7.1Γ—10βˆ’14p = 7.1 \times 10^{-14}p=5.3Γ—10βˆ’12p = 5.3 \times 10^{-12}

‑ Tests 10–12 depend on planet identity (mirror-pair assignments, period fractions, dd-assignments), not on reshuffled values, so the permutation null cannot test them. The Monte Carlo nulls generate fully random assignments and give meaningful pp-values.

Eight tests reach p<0.05p < 0.05 across all applicable null distributions: pairwise Fibonacci count, inclination balance, eccentricity balance, Saturn prediction, the full ψ\psi-constant, the R2R^2 partition, the E–J–S resonance, and mirror symmetry. The overall structure is highly significant (Fisher’s combined p≀7.1Γ—10βˆ’14p \leq 7.1 \times 10^{-14} in Monte Carlo, p=1.4Γ—10βˆ’5p = 1.4 \times 10^{-5} in the conservative permutation test), robust across all three null distributions.

Tests 2–4 and 9 are individually non-significant, as expected: the eccentricity ladder involves only 4 inner planets (limited statistical power), Tests 3–4 suffer from circularity with model-derived amplitudes, and the precession hierarchy count is not discriminating because many random period sets also produce Fibonacci-like ratios among 10+ pairs.


Exoplanet Tests: TRAPPIST-1 and Kepler-90

TRAPPIST-1 period ratios β€” strong Fibonacci content

Five of six adjacent period ratios involve only Fibonacci numbers: 8:5, 5:3, 3:2, 3:2, 3:2 (only f:g β‰ˆ\approx 4:3 uses non-Fibonacci 4). This gives 83% Fibonacci content β€” identical to the Solar System’s 83%.

TRAPPIST-1 additive triad

The mass-weighted eccentricity ΞΎ=em/M⋆\xi = e\sqrt{m/M_\star} yields a Fibonacci additive triad: 3ΞΎb+5ΞΎg=8ΞΎe3\xi_b + 5\xi_g = 8\xi_e at 0.34% error β€” using the same Fibonacci triple (3, 5, 8) that appears in the Solar System’s period denominators for Earth, Jupiter, and Saturn. Additional triads include ΞΎd+ΞΎh=2ΞΎe\xi_d + \xi_h = 2\xi_e (0.40%) and ΞΎe+ΞΎf=2ΞΎb\xi_e + \xi_f = 2\xi_b (0.51%).

TRAPPIST-1 super-period β€” the 311 connection

The optimal integer multiplier NN of PbP_b where all 7 planet periods divide near-evenly (max deviation 0.12%) is N=311N = 311, the same number as the Solar System master ratio R=ψ/ΞΎVβ‰ˆ310.9R = \psi/\xi_V \approx 310.9.

Monte Carlo significance: Generating 10510^5 random Fibonacci-chain 7-planet systems, only 0.13% select N=311N = 311. The probability that both the Solar System and TRAPPIST-1 independently select 311 is ∼2Γ—10βˆ’6\sim 2 \times 10^{-6} β€” highly significant.

TRAPPIST-1i candidate planet

A candidate 8th planet with Pβ‰ˆ28.7P \approx 28.7 days has been identified (JWST 2025, tentative), in 3:2 resonance with planet h. If confirmed, TRAPPIST-1 would have 6/7=86%6/7 = 86\% Fibonacci-only period ratios.

TRAPPIST-1 limitations

Both systems show ~83% Fibonacci period ratios and both select 311. However, TRAPPIST-1’s eccentricities are extremely small (~0.002–0.01) with narrow dynamic range (4Γ—4\times vs Solar System’s 141Γ—141\times), making ΞΎ\xi-ladder tests impractical. Transit inclinations measure viewing geometry, not dynamical amplitudes. Deeper tests require systems with independently measured eccentricities and TTV-measured masses for 4+ planets.

Kepler-90 β€” limited by data

Only 2 of 8 planets have TTV-measured masses and eccentricities. Period ratios show 71% Fibonacci content (5/7 adjacent pairs).

Comparative summary

SystemPlanetsPeriod-Fibonacci %ΞΎ\xi-Fibonacci %
Solar System871% (5/7)33% (7/21 pairs)
TRAPPIST-1783% (5/6)38% (8/21 pairs)
Kepler-90871% (5/7)insufficient data

Relation to Prior Work and What’s Novel

Existing Fibonacci research in planetary science

Molchanov (1968) β€” Integer resonances in orbital frequencies

Molchanov proposed that planetary orbital frequencies satisfy simultaneous linear equations with small integer coefficients. His framework used general small integers β€” not specifically Fibonacci numbers β€” and dealt exclusively with orbital frequencies. He did not incorporate planetary masses, eccentricities, or inclinations.

Key difference: Molchanov found approximate integer relations among frequencies. Our laws use specifically Fibonacci numbers, applied to mass-weighted eccentricities and inclinations.

Aschwanden (2018) β€” Harmonic resonances in orbital spacing

Aschwanden identified five dominant harmonic ratios governing planet and moon orbit spacing, achieving ~2.5% accuracy on semi-major axis predictions. The analysis is purely kinematic β€” planetary mass, eccentricity, and inclination do not appear.

Key difference: Aschwanden analyzed distance/period ratios between consecutive pairs. Our laws analyze mass-weighted values of individual planets.

Pletser (2019) β€” Fibonacci prevalence in period ratios

Pletser found ~60% alignment of period ratios with Fibonacci fractions, with the tendency increasing for minor planets with smaller eccentricities and inclinations. He used eccentricity and inclination only as selection filters.

Key difference: Pletser did not analyze whether eccentricities or inclinations themselves form Fibonacci ratios. Mass-weighting is entirely absent. None of our six laws appear in his analysis.

Comparison table

AspectMolchanov (1968)Aschwanden (2018)Pletser (2019)This work
ParametersFrequencies onlyPeriods/distancesPeriod ratiosEccentricity, inclination, mass
What is comparedLinear frequency sumsConsecutive pair ratiosPairwise period ratiosMass-weighted individual values
Uses mass?NoNoNoYes (m\sqrt{m})
Uses eccentricity?NoNoAs filter onlyYes (primary variable)
Predicts elements?NoDistances onlyNoYes (eccentricities, inclinations)

What builds on established theory

Law 1 (Fibonacci Cycle Hierarchy) builds on the known precession periods of the planets. The individual periods are established results of celestial mechanics β€” what is new is recognizing them as a single Fibonacci-divided hierarchy rooted in a master timescale HH.

Law 3 (Inclination Balance) is rooted in angular momentum conservation. The weight factor mβ‹…a(1βˆ’e2)\sqrt{m \cdot a(1-e^2)} is proportional to a planet’s orbital angular momentum LL. The invariable plane is defined as the plane perpendicular to the total angular momentum vector, so inclination oscillations must balance around it β€” that is what makes it the invariable plane. The novel contribution is that dividing by a Fibonacci divisor dd preserves the balance to 99.9998%.

Phase angles (203.3195Β° and 23.3195Β°) originate from the s8s_8 eigenmode of Laplace-Lagrange secular perturbation theory, a framework established in classical celestial mechanics (18th–19th century). Saturn’s retrograde ascending node precession is also a known result from secular theory.

Law 5 (Eccentricity Balance) connects to Angular Momentum Deficit (AMD) conservation, a known conserved quantity in secular theory. The weight mΓ—a3/2Γ—e/d\sqrt{m} \times a^{3/2} \times e / \sqrt{d} contains factors related to how AMD is partitioned among planets. However, the linear dependence on eccentricity (rather than quadratic, as in the AMD itself) and the 1/d1/\sqrt{d} scaling distinguish it from the standard AMD formulation.

Law 6 (Saturn-Jupiter-Earth Resonance) describes beat frequency relationships between known precession periods. The individual periods are well-established β€” the closed-loop structure connecting them through Fibonacci addition is the novel observation.

What’s novel

  1. Fibonacci division of a single timescale β€” all major precession periods equal H/F(n)H/F(n) for successive Fibonacci numbers
  2. Mass-weighted orbital parameters as Fibonacci variables β€” ΞΎ=XΓ—m\xi = X \times \sqrt{m} connects Fibonacci structure to physical properties, not just orbital timing
  3. Fibonacci structure in eccentricities and inclinations β€” extends Fibonacci from one orbital element (period) to three
  4. Pure Fibonacci divisors with exact mirror symmetry β€” all 8 divisors are Fibonacci numbers, forming 4 symmetric pairs across the asteroid belt
  5. Zero-free-parameter inclination predictions β€” ψ=F5Γ—F82/(2H)\psi = F_5 \times F_8^2 / (2H) gives a single universal constant that predicts all 8 planets from HH alone
  6. Zero-free-parameter eccentricity predictions β€” AMD partition ratios satisfy Fibonacci pair constraints, determining all 8 eccentricities from inclinations
  7. Configuration uniqueness β€” the mirror-symmetric solution is the unique configuration satisfying all 4 physical constraints out of 7.5 million tested
  8. Eccentricity balance β€” an independent balance condition on eccentricities using the same divisors
  9. Saturn eccentricity prediction β€” a direct consequence of Saturn’s unique retrograde status
  10. Closed resonance loop β€” Saturn-Jupiter-Earth beat frequencies form a triangle that is an algebraic consequence of Fibonacci addition

Assessment

The balance conditions (Laws 3 and 5) combine known conservation principles with a novel Fibonacci structure that modulates the planetary weights. The conservation laws guarantee that inclination and eccentricity oscillations balance around the invariable plane β€” but they do not predict that integer Fibonacci divisors should preserve that balance to such high precision. Law 2 (Inclination Amplitude quantization) and Law 4 (Eccentricity Constant) are the most genuinely novel claims β€” no existing theory predicts that dΓ—amplitudeΓ—md \times \text{amplitude} \times \sqrt{m} should be constant across all planets, or that AMD partition ratios within mirror pairs should satisfy specific Fibonacci fractions.

The key unresolved question is why Fibonacci numbers work: do they encode something about the secular eigenmode structure (real physics), or is the Fibonacci restriction a coincidence made possible by having enough number choices? The mirror symmetry and the triple-constraint uniqueness of Config #32 argue against coincidence, but a theoretical derivation from first principles β€” or a successful prediction for an independent system such as exoplanetary or satellite systems β€” would be needed to settle the question definitively.


Open Questions

  1. RΒ² Fibonacci targets β€” Partially resolved. Law 4 uses eight specific Fibonacci fractions (four R2R^2 sums and four products/ratios) to predict all eccentricities. Exhaustive search finds no rule generating these targets from pair properties β€” the Fibonacci indices appear to be irreducible data. Whether they can be derived from a single structural principle remains open.

  2. Physical derivation of eccentricity balance β€” The inclination balance follows from angular momentum conservation. What conservation law or secular perturbation mechanism produces the eccentricity balance? The linear (rather than quadratic) dependence on ee distinguishes it from AMD conservation.

  3. Universality β€” Do the balance conditions hold for other planetary systems, or are they specific to the solar system’s Fibonacci divisor structure? TRAPPIST-1 shows promising Fibonacci content (83% period ratios, 311 super-period) but lacks the mass and eccentricity data needed to test the balance conditions.

  4. The master ratio Rβ‰ˆ311R \approx 311 β€” Why does the formation-epoch eccentricity scale land near a Fibonacci primitive root prime? Whether formation generically converges toward FPR primes (via KAM attractor dynamics) remains open.


References

Fibonacci and orbital resonance

  1. Molchanov, A.M. (1968). β€œThe resonant structure of the Solar System.” Icarus, 8(1-3), 203-215. ScienceDirectΒ 
  2. Backus, G.E. (1969). β€œCritique of β€˜The Resonant Structure of the Solar System’ by A.M. Molchanov.” Icarus, 11, 88-92.
  3. Molchanov, A.M. (1969). β€œResonances in complex systems: A reply to critiques.” Icarus, 11(1), 95-103.
  4. Aschwanden, M.J. (2018). β€œSelf-organizing systems in planetary physics: Harmonic resonances of planet and moon orbits.” New Astronomy, 58, 107-123. arXivΒ 
  5. Aschwanden, M.J., & Scholkmann, F. (2017). β€œExoplanet Predictions Based on Harmonic Orbit Resonances.” Galaxies, 5(4), 56. MDPIΒ 
  6. Pletser, V. (2019). β€œPrevalence of Fibonacci numbers in orbital period ratios in solar planetary and satellite systems and in exoplanetary systems.” Astrophysics and Space Science, 364, 158. arXivΒ 

KAM theory and orbital stability

  1. Kolmogorov, A.N. (1954). β€œOn the conservation of conditionally periodic motions under small perturbation of the Hamiltonian.” Doklady Akad. Nauk SSSR, 98, 527-530.
  2. Arnold, V.I. (1963). β€œProof of a theorem of A.N. Kolmogorov on the invariance of quasi-periodic motions under small perturbations of the Hamiltonian.” Russian Math. Surveys, 18(5), 9-36.
  3. Greene, J.M. (1979). β€œA method for determining a stochastic transition.” J. Math. Phys., 20, 1183-1201.
  4. Morbidelli, A., & Giorgilli, A. (1995). β€œSuperexponential stability of KAM tori.” J. Stat. Phys., 78, 1607-1617.
  5. Laskar, J. (1989). β€œA numerical experiment on the chaotic behaviour of the Solar System.” Nature, 338, 237-238.
  6. Celletti, A., & Chierchia, L. (2007). β€œKAM stability and celestial mechanics.” Memoirs of the AMS, 187.

Exoplanet data

  1. Agol, E., et al. (2021). β€œRefining the Transit-timing and Photometric Analysis of TRAPPIST-1.” Planetary Science Journal, 2, 1. arXivΒ 
  2. Grimm, S.L., et al. (2018). β€œThe nature of the TRAPPIST-1 exoplanets.” Astronomy & Astrophysics, 613, A68.

Computational verification

The following scripts verify the laws documented above:

  • fibonacci_data.py β€” Shared constants: planetary data (Holistic computation chain), Fibonacci sequences, divisor assignments, law verification functions
  • fibonacci_significance.py β€” Monte Carlo and permutation significance tests (12 tests, 3 null distributions)
  • fibonacci_311_analysis.py β€” Master ratio analysis, Pisano period, AMD connection, optimal mass exponent
  • fibonacci_311_deep.py β€” Deep 311 investigation: FPR prime class, two-layer explanation, TRAPPIST-1 connection
  • fibonacci_exoplanet_test.py β€” Exoplanet tests: TRAPPIST-1 and Kepler-90
  • fibonacci_trappist1_deep.py β€” TRAPPIST-1 deep analysis: candidate planet i, super-period significance
  • fibonacci_j2000_eccentricity.py β€” Eccentricity ladder formation constraint analysis (Monte Carlo, AMD)
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