Sun Synchronous Orbit Inclination Formula:
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A Sun Synchronous Orbit (SSO) is a nearly polar orbit where the satellite passes over any given point of the planet's surface at the same local solar time. This provides consistent lighting conditions for Earth observation and remote sensing applications.
The calculator uses the Sun Synchronous Orbit inclination formula:
Where:
Explanation: The formula calculates the inclination needed for the orbital plane to precess at the same rate as the Earth orbits the Sun, maintaining constant solar illumination angles.
Details: SSOs are crucial for Earth observation satellites, weather monitoring, environmental studies, and military reconnaissance as they provide consistent lighting conditions and regular coverage of the entire Earth's surface.
Tips: Enter semi-major axis in km, precession rate in deg/day (default 0.9856 for sun sync), Earth radius in km (default 6371), and J2 coefficient (default 0.0010826). All values must be positive.
Q1: What is the typical altitude range for sun synchronous orbits?
A: Most sun synchronous orbits are between 600-800 km altitude, corresponding to inclinations of approximately 97-98 degrees.
Q2: Why is the inclination greater than 90 degrees?
A: Sun synchronous orbits are retrograde orbits (inclination > 90°) to achieve the required precession rate for synchronization with the Sun.
Q3: How does J2 affect the orbit?
A: J2 represents Earth's oblateness and causes the orbital plane to precess. This effect is exploited to create sun synchronous orbits.
Q4: Can this formula be used for other planets?
A: Yes, but you would need to use the appropriate values for that planet's radius, gravitational parameter, and J2 coefficient.
Q5: What happens if the calculated inclination is outside 0-180 degrees?
A: The formula should always yield a valid inclination between 0-180 degrees for physically possible parameters. If not, check your input values.