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Heliosynchronous orbit

 
Military Dictionary: sun-synchronous orbit

(DOD) An orbit in which the satellite's orbital plane is at a fixed orientation to the sun, i.e., the orbit precesses about the earth at the same rate that the earth orbits the sun. It has the characteristics of maintaining similar sun angles along its ground trace for all orbits, and typically has an inclination from 96 to 98 degrees, depending on the orbit altitude and orbit shape (eccentricity). See also synchronous orbit.

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Wikipedia: Heliosynchronous orbit
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This article is about a class of orbits about the sun. For a class of orbits around the earth, see sun-synchronous orbit.

By analogy with the geosynchronous orbit, a heliosynchronous orbit is a heliocentric orbit where the satellite's period of revolution matches the Sun's period of rotation. These orbits occur at a radius of 24.360 Gm (0.1628 AU) around the Sun, a little less than half of the orbital radius of Mercury.

Similar to the geostationary orbit, the heliostationary orbit is the heliosynchronous orbit of inclination zero and eccentricity zero, so that the satellite would appear stationary to an observer on the Sun's surface.

To date, no satellites have been put in this kind of solar orbit.

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Copyrights:

Military Dictionary. US Department of Defense Dictionary of Military and Associated Words, 2003.  Read more
Wikipedia. This article is licensed under the Creative Commons Attribution/Share-Alike License. It uses material from the Wikipedia article "Heliosynchronous orbit" Read more