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1Understand the Formula
🛠️ Step 1: Understand the Formula
The core formula is:
m = NKTg₁ / (x × v)
where NKTg₁ = x × m × v
(Note:p = m × vandxis heliocentric distance in km)You can rearrange the formula to solve for
mifNKTg₁,x, andvare known.🌐 Step 2: Get Real Planetary Data
Go to NASA JPL Horizons and extract the following for each planet:
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Heliocentric distance
xin kilometers (use vector magnitude) -
Orbital velocity
vin km/s -
Official mass
m(optional, for comparison only)
Date used in this experiment: 30–31 December 2024
You can choose your own date, but use the same timestamp for all values.🧮 Step 3: Calculate NKTg₁
Use the known mass
m, positionx, and velocityvto compute:NKTg₁ = x × m × v
Store this value — it becomes your interpolation key.
🧪 Step 4: Interpolate Mass
Once you have
x,v, andNKTg₁, use the interpolation formula:m = NKTg₁ / (x × v)
You should get back the original mass with extremely high accuracy (Δm ≈ 0).
If not, check your unit consistency (use SI base units: kg, km, s).📐 Step 5: Verify with NASA Data
Compare your interpolated mass with official values from:
Typical expected error: < 0.0001>#/strong###
🌍 Step 6 (Optional): Detect Earth’s Mass Loss
You can apply the model across multiple dates in a year to detect mass variation on Earth. Use real GRACE-based timestamps, and compare:
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Interpolated
mover time -
Known mass loss from GRACE (10²⁰–10²¹ kg/year)
Even very small differences will appear in the model due to its high sensitivity.
🧠 Notes
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This model assumes Newtonian orbital mechanics (no GR corrections).
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Unit consistency is critical: km, km/s, and kg throughout.
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You can automate calculations in Excel, Python, or Jupyter Notebooks.
📁 Files & Tools
(Add links in Files tab once available)
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✅ Example spreadsheet (
NKTg_Interpolation.xlsx
) Experimental Verification of the NKT Law Interpolating the Masses of 8 Planets Using NASA Data as of 30–31122024 SHA256 a08c424e2259803a2b10d8d51d61ee4b9073f2b9a62111e4858abf0839229320.pdf
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Nguyen Khanh Tung
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