3D Orbital Period Calculation
This 3D simulation demonstrates the conversion of the constant k and calculation of the Moon's orbital period around Earth.
Example
Question:
Express the constant \(k\) of Eq. (7.38) in days and kilometres. Given \(k = 10^{-13}\;\mathrm{s}^2\,\mathrm{m}^{-3}\). The moon is at a distance of \(3.84 \times 10^5\,\mathrm{km}\) from the earth. Obtain its time-period of revolution in days.
Solution:
Given: \[ k = 10^{-13}\;\mathrm{s}^2\,\mathrm{m}^{-3} \] To convert \(k\) to days and kilometres: \[ k = 10^{-13}\left[\frac{1}{(24 \times 60 \times 60)^2}\right]\left[\frac{1}{(1/1000)^3}\right]\,\mathrm{d}^2\,\mathrm{km}^{-3} \] \[ = 1.33 \times 10^{-14}\;\mathrm{d}^2\,\mathrm{km}^{-3} \] Using Eq. (7.38) with this value: \[ T^2 = (1.33 \times 10^{-14})(3.84 \times 10^5)^3 \] \[ T = 27.3\,\mathrm{d} \] Note: Eq. (7.38) also holds for elliptical orbits if we replace \((R_E + h)\) by the semi-major axis of the ellipse. The earth will then be at one of the foci of this ellipse.
Conversion of Constant k
We need to express k in days and kilometres:
= 10⁻¹³ [1/(24 × 60 × 60)² d²] [1/(1/1000)³ km⁻³]
= 1.33 × 10⁻¹⁴ d² km⁻³
1 day = 24 × 60 × 60 = 86400 seconds
1 km = 1000 meters
Therefore:
1 s = 1/86400 d
1 m = 1/1000 km
Calculation of Moon's Orbital Period
Using the relationship T² = kR³ (Kepler's Third Law):
T² = (1.33 × 10⁻¹⁴) × (5.66 × 10¹⁶)
T² ≈ 753.33 d²
T ≈ √753.33 ≈ 27.3 days
Key Notes
1. The same relationship holds for elliptical orbits if we replace the distance with the semi-major axis of the ellipse.
2. For elliptical orbits, Earth would be at one of the foci of the ellipse.
3. The animation above shows the Moon's orbit (simplified as circular) with the correct 27.3 day period.



