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Calcimator

Orbital Mechanics Calculator

Complete orbital mechanics calculations. Kepler's laws, Hohmann transfers, delta-v, Lagrange points, escape velocities, and relativistic effects.

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How to Use This Calculator
  1. Use the Kepler module to enter semi-major axis (AU) and central mass (solar masses) to compute Orbital Period and Mean Velocity.
  2. In the Hohmann Transfer section, enter departure and arrival orbit radii to get Total Delta-V (km/s) and Transfer Time (days).
  3. Check Lagrange Points to find stable gravitational equilibria — L4 and L5 are stable, L1/L2/L3 are unstable.
  4. Use the Roche Limit and Hill Sphere outputs to determine where a satellite will survive vs. be tidally disrupted.
  5. Review the orbital comparison chart against the solar system planets to contextualize your orbit.

What each input means

Calculation Type
Calculation mode to use.
Central Body Mass (M☉)
Mass in solar masses
Semi-Major Axis (AU)
Average orbital distance
Eccentricity
0 = circle, <1 = ellipse, 1 = parabola
Inclination (degrees)
Angle from reference plane
Starting Orbit (AU)
Earth orbit = 1 AU
Target Orbit (AU)
Mars orbit ≈ 1.52 AU
Parent Body Mass (Earth masses)
Sun ≈ 333,000 Earth masses
Primary Mass (M☉)
Larger body (e.g., Sun)
Secondary Mass (M☉)
Smaller body (Earth ≈ 3e-6 M☉)
Orbital Radius (AU)
Mercury ≈ 0.387 AU
Object Velocity (km/s)
Mercury ≈ 47.87 km/s

How this is calculated

Formula

T² = (4π²/GM)a³ (Kepler's 3rd) | v = √(GM/r) | ΔV = v_transfer - v_circular

Worked example, using the default values

  1. Identify Input Parameters
    4 parameters
    Calculation Type = 0, Central Body Mass (M☉) = 1, Semi-Major Axis (AU) = 1, Eccentricity = 0.017 = 18 input(s) provided
  2. Calculate Orbital Period
    Orbital Period
    0.9998918722467838 = 0.9998918722467838
  3. Calculate Mean Velocity
    Mean Velocity
    29.7888993205065 = 29.7888993205065
  4. Calculate Orbital Period
    Orbital Period
    365.21050633813775 = 365.21050633813775
  5. Calculate Perihelion
    Perihelion
    0.983 = 0.983

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