Free Specific Orbital Energy Calculator
Find the specific mechanical energy of an orbit: epsilon = -G M / (2a).
m
kg
Specific Orbital Energy
-29,432,232 J/kg
Specific Orbital Energy vs Semi-Major Axis
Specific Orbital Energy
epsilon = -G M / (2a)
This quantity is constant along the entire Keplerian orbit.
Example Calculation
ISS orbit with semi-major axis a = 6 771 km around Earth.
- 01epsilon = -G M / (2a)
- 02G M = 3.986e14
- 032a = 1.354e7
- 04epsilon = -3.986e14 / 1.354e7 ≈ -29.4 MJ/kg