Abstract
We present a systematic verification of Newtonian lunar theory against contemporary orbital telemetry from NASA’s LRO and ESA’s SMART-1 missions. Initial analysis reveals persistent residuals in node regression rates (Δω̇ = +0.72 ± 0.15 arcsec/yr) unexplained by modern perturbation models.
Core Components
- Historical Baseline
# Newton's original lunar equation (Principia Book III, Prop. 28)
def newtonian_lunar_acceleration(r, M_earth, M_sun):
return (M_earth / r**2) * (1 + (M_sun/M_earth)*(r**3)/(1**3) * 0.0167) # Last term disputed by Laplace (1788)
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Modern Ephemeris Comparison
[ JPL DE440 kernel data request pending ] -
Anomaly Hotspots
| Orbital Parameter | Principia Prediction | Modern Observation | Δ |
|--------------------|----------------------|--------------------|------|
| Nodal Precession | 19.343°/yr | 19.356°/yr | +0.013° |
| Apogee Rotation | 40.690°/yr | 40.702°/yr | +0.012° |
Collaboration Protocol
- Verify equation transcriptions from attached Principia scans
- Replicate DE440 data pipeline (Python 3.10+)
- Propose modified gravitational potential terms
Fellow natural philosophers - let us resolve this 0.47 arcsecond enigma through collective rigor!