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  2. Sun-synchronous orbit - Wikipedia

    en.wikipedia.org/wiki/Sun-synchronous_orbit

    i is the inclination of the orbit to the equator. An orbit will be Sun-synchronous when the precession rate ρ = ⁠ d Ω d t⁠ equals the mean motion of the Earth about the Sun nE, which is 360° per sidereal year (1.990 968 71 × 10−7 rad /s), so we must set nE = ⁠ Δ ΩE TE⁠ = ρ = ⁠ Δ Ω T⁠ , where TE is the earth orbital period ...

  3. Low Earth orbit - Wikipedia

    en.wikipedia.org/wiki/Low_Earth_orbit

    A wide variety of sources [4] [5] [6] define LEO in terms of altitude.The altitude of an object in an elliptic orbit can vary significantly along the orbit. Even for circular orbits, the altitude above ground can vary by as much as 30 km (19 mi) (especially for polar orbits) due to the oblateness of Earth's spheroid figure and local topography.

  4. List of orbits - Wikipedia

    en.wikipedia.org/wiki/List_of_orbits

    Average altitude of 384,403 kilometres (238,857 mi), elliptical-inclined orbit. Beyond-low Earth orbit (BLEO) and beyond Earth orbit (BEO) are a broad class of orbits that are energetically farther out than low Earth orbit or require an insertion into a heliocentric orbit as part of a journey that may require multiple orbital insertions ...

  5. Beta angle - Wikipedia

    en.wikipedia.org/wiki/Beta_angle

    In orbital mechanics, the beta angle ( ) is the angle between a satellite 's orbital plane around Earth and the geocentric position of the Sun. [1] The beta angle determines the percentage of time that a satellite in low Earth orbit (LEO) spends in direct sunlight, absorbing solar radiation. [2] For objects launched into orbit, the solar beta ...

  6. Polar orbit - Wikipedia

    en.wikipedia.org/wiki/Polar_orbit

    The half-orbit on the Sun side then takes only 50 minutes, during which local time of day does not vary greatly. To retain a Sun-synchronous orbit as the Earth revolves around the Sun during the year, the orbit must precess about the Earth at the same rate (which is not possible if the satellite passes directly over the pole). Because of Earth ...

  7. Orbital inclination - Wikipedia

    en.wikipedia.org/wiki/Orbital_inclination

    Orbits. The inclination is one of the six orbital elements describing the shape and orientation of a celestial orbit. It is the angle between the orbital plane and the plane of reference, normally stated in degrees. For a satellite orbiting a planet, the plane of reference is usually the plane containing the planet's equator.

  8. Medium Earth orbit - Wikipedia

    en.wikipedia.org/wiki/Medium_Earth_orbit

    Medium Earth orbit. Space of Medium Earth orbits (MEO) as pink area, with Earth and the distance of the orbit of the Moon for reference and to scale. A medium Earth orbit (MEO) is an Earth-centered orbit with an altitude above a low Earth orbit (LEO) and below a high Earth orbit (HEO) – between 2,000 and 35,786 km (1,243 and 22,236 mi) above ...

  9. Synchronous orbit - Wikipedia

    en.wikipedia.org/wiki/Synchronous_orbit

    Synchronous orbit. Orbit of an astronomical body equal to that body's average rotational period. A synchronous orbit is an orbit in which an orbiting body (usually a satellite) has a period equal to the average rotational period of the body being orbited (usually a planet), and in the same direction of rotation as that body. [1]