Polar orbit

From Wikipedia, the free encyclopedia

Jump to: navigation, search

A polar orbit is an orbit in which a satellite passes above or nearly above both poles of the body (usually a planet such as the Earth, but possibly another body such as the Sun) being orbited on each revolution. It therefore has an inclination of (or very close to) 90 degrees to the equator. Except in the special case of a polar geosynchronous orbit, a satellite in a polar orbit will pass over the equator at a different longitude on each of its orbits.

Polar orbits are often used for earth-mapping-, earth observation- and reconnaissance satellites, as well as some weather satellites. The disadvantage to this orbit is that no one spot on the Earth's surface can be sensed continuously from a satellite in a polar orbit.

A satellite can hover over one polar area a large part of the time, albeit at a large distance, using a polar highly elliptical orbit with its apogee above that area. This is the principle behind a Molniya orbit.

[edit] See also

[edit] External links


bg:Полярна орбита

ca:Òrbita polar cs:Polární dráha es:Órbita polar fr:Orbite polaire it:Orbita polare hu:Poláris pálya no:Polarbane nn:Polarbane pt:Órbita polar sk:Polárna dráha

Views
Personal tools

Toolbox