geosynchronous earth orbit
1Medium Earth orbit — MEO redirects here. For other uses, see MEO (disambiguation). Comparison of GPS, GLONASS, Galileo and Compass (medium earth orbit) satellite navigation system orbits with the International Space Station, Hubble Space Telescope and Iridium… …
2Low Earth Orbit — Ein Satellitenorbit ist die Umlaufbahn eines Satelliten um die Erde. Dieser Artikel befasst sich mit der Flughöhe. Zur genauen Beschreibung der Flugbahn bedarf es weiterer Kenngrößen, die die Artikel Bahnelemente und Satellitenbahnelemente… …
3Medium Earth Orbit — Ein Satellitenorbit ist die Umlaufbahn eines Satelliten um die Erde. Dieser Artikel befasst sich mit der Flughöhe. Zur genauen Beschreibung der Flugbahn bedarf es weiterer Kenngrößen, die die Artikel Bahnelemente und Satellitenbahnelemente… …
4Low Earth orbit — An orbiting cannon ball showing various sub orbital and orbital possibilities …
5Medium Earth Orbit — (MEO), sometimes called Intermediate Circular Orbit (ICO), is the region of space around the Earth above low Earth orbit (convert|2000|km|mi|0) and below geostationary orbit (convert|35786|km|mi|0). [ [http://e words.us/w/MEO.html MEO… …
6High Earth orbit — A High Earth Orbit is a geocentric orbit whose apogee lies above that of a geosynchronous orbit (35,786 km) [ [http://gcmd.nasa.gov/User/suppguide/platforms/orbit.html Orbit ] ] .Highly Elliptical Orbits are generally considered to be a subset of …
7Geosynchronous satellite — A geosynchronous satellite is a satellite whose orbital track on the Earth repeats regularly over points on the Earth over time. If such a satellite s orbit lies over the equator and the orbit is circular, it is called a geostationary satellite.… …
8Orbit — This article is about orbits in celestial mechanics, due to gravity. For other uses, see Orbit (disambiguation). A satellite orbiting the Earth has a tangential velocity and an inward acceleration …
9Geosynchronous Satellite Launch Vehicle — Infobox rocket name = GSLV imsize = 250 caption = Geosynchronous Satellite Launch Vehicle function = Expendable launch vehicle manufacturer = ISRO country origin = IND height = 49 m alt height = 160 ft diameter = 2.8 m alt diameter = 9.1 ft mass …
10Orbit equation — In astrodynamics an orbit equation defines the path of orbiting body around central body relative to , without specifying position as a function of time. Under standard assumptions, a body moving under the influence of a force, directed to a… …
