Earth's Orbit
Semi-major axis (a): 149,600,000,000 m; Standard gravitational parameter (μ): 132,700,000,000,000,000,000 m³/s²
Orbital Period (seconds): 31,560,349.01 s; Orbital Period (days): 365.2818173 days
Calculates the time it takes for an object to complete one orbit around another object using Kepler's Third Law.
Start with your values, or try a preset.
Enter Semi-major axis (a) and Standard gravitational parameter (μ) in the units shown.
Read Orbital Period (seconds) and Orbital Period (days) in the results panel. Results update as you change the inputs.
Choose a preset to load an example, then adjust the values for your situation.
See the inputs and their calculated results.
Semi-major axis (a): 149,600,000,000 m; Standard gravitational parameter (μ): 132,700,000,000,000,000,000 m³/s²
Orbital Period (seconds): 31,560,349.01 s; Orbital Period (days): 365.2818173 days
Semi-major axis (a): 384,400,000 m; Standard gravitational parameter (μ): 132,700,000,000,000,000,000 m³/s²
Orbital Period (seconds): 4,110.73495 s; Orbital Period (days): 0.04757795081 days
Semi-major axis (a): 227,900,000,000 m; Standard gravitational parameter (μ): 132,700,000,000,000,000,000 m³/s²
Orbital Period (seconds): 59,341,824.48 s; Orbital Period (days): 686.8266722 days
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