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)

  • Negative energy = bound (elliptical) orbit
  • Zero = parabolic escape
  • Positive = hyperbolic trajectory
  • This quantity is constant along the entire Keplerian orbit.

    Example Calculation

    ISS orbit with semi-major axis a = 6 771 km around Earth.

    1. 01epsilon = -G M / (2a)
    2. 02G M = 3.986e14
    3. 032a = 1.354e7
    4. 04epsilon = -3.986e14 / 1.354e7 ≈ -29.4 MJ/kg

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