SSO Inclination Formula:
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The SSO (Sun-Synchronous Orbit) inclination formula calculates the orbital inclination required for a satellite to maintain a sun-synchronous orbit. This type of orbit allows a satellite to pass over any given point on Earth at the same local solar time.
The calculator uses the SSO inclination formula:
Where:
Explanation: The formula calculates the precise orbital inclination needed to maintain sun-synchronization based on the Earth's oblateness and the satellite's orbital characteristics.
Details: Accurate SSO inclination calculation is crucial for Earth observation satellites, weather monitoring, and remote sensing missions where consistent lighting conditions are essential for data comparison over time.
Tips: Enter the flattening coefficient and orbital eccentricity as unitless values. Ensure that f/(2×e²) is between -1 and 1 for a valid result.
Q1: What is a sun-synchronous orbit?
A: A sun-synchronous orbit is a nearly polar orbit where the satellite's orbital plane precesses at the same rate as the Earth's revolution around the sun, maintaining constant solar illumination angles.
Q2: What are typical values for flattening and eccentricity?
A: For Earth, the flattening coefficient is approximately 0.003353. Eccentricity for sun-synchronous orbits is typically very small, often close to zero for near-circular orbits.
Q3: Why does the formula use arccos?
A: The arccos function calculates the angle whose cosine equals the expression, converting the ratio into an inclination angle measured in degrees.
Q4: What happens if f/(2×e²) is outside the range [-1, 1]?
A: The calculation becomes invalid as the arccos function is only defined for values between -1 and 1 inclusive.
Q5: Can this formula be used for other planets?
A: Yes, but with appropriate flattening and eccentricity values specific to the celestial body in question.