SatellitenOrbits
SatellitenOrbits are the paths followed by artificial satellites as they travel around a planet or moon under the influence of gravity. In the simplest model, motion is described by Newton's law of gravitation and follows a conic section, with a circular orbit as a special case of minimum energy. The two-body approximation treats the satellite and central body while neglecting other gravitational influences, though real orbits are perturbed by the Moon and Sun, atmospheric drag, and the planet’s oblateness.
Orbits are commonly categorized by altitude and energy: low Earth orbit (LEO) up to about 2,000 kilometers
Each orbit is described by six classical orbital elements: semi-major axis (a), eccentricity (e), inclination (i),
Over time, perturbations alter the orbit. Atmospheric drag shrinks altitude in LEO; Earth's equatorial bulge causes
Applications span communications, weather and Earth observation, navigation, and science missions. GEO satellites provide fixed-area coverage;