- Low Earth orbit
A low Earth orbit (LEO) is generally defined as an orbit within the locus extending from the Earth’s surface up to an altitude of 2,000 km. Given the rapid orbital decay of objects below approximately 200 km, the commonly accepted definition for LEO is between 160–2,000 km (100–1,240 miles) above the Earth's surface.
With the exception of the lunar flights of the Apollo program, all human spaceflights have either been orbital in LEO or sub-orbital. The altitude record for a human spaceflight in LEO was Gemini 11 with an apogee of 1,374.1 km.
Objects in LEO encounter atmospheric drag in the form of gases in the thermosphere (approximately 80–500 km up) or exosphere (approximately 500 km and up), depending on orbit height. LEO is an orbit around Earth between the atmosphere and below the inner Van Allen radiation belt. The altitude is usually not less than 300 km because that would be impractical due to the larger atmospheric drag.
Equatorial low Earth orbits (ELEO) are a subset of LEO. These orbits, with low inclination to the Equator, allow rapid revisit times and have the lowest delta-v requirement of any orbit. Orbits with a high inclination angle are usually called polar orbits.
Higher orbits include medium Earth orbit (MEO), sometimes called intermediate circular orbit (ICO), and further above, geostationary orbit (GEO). Orbits higher than low orbit can lead to early failure of electronic components due to intense radiation and charge accumulation.
While a majority of artificial satellites are placed in LEO, where they travel at about 7.8 km/s (28,080 km/h), making one complete revolution around the Earth in about 90 minutes, many communication satellites require geostationary orbits, and move at the same angular velocity as the Earth. Since it requires less energy to place a satellite into a LEO and the LEO satellite needs less powerful amplifiers for successful transmission, LEO is still used for many communication applications. Because these LEO orbits are not geostationary, a network (or "constellation") of satellites is required to provide continuous coverage. Lower orbits also aid remote sensing satellites because of the added detail that can be gained. Remote sensing satellites can also take advantage of sun-synchronous LEO orbits at an altitude of about 800 km (500 mi) and near polar inclination. ENVISAT is one example of an Earth observation satellite that makes use of this particular type of LEO.
Although the Earth's pull due to gravity in LEO is not much less than on the surface of the Earth, people and objects in orbit experience weightlessness due to the effects of freefall.
The LEO environment is becoming congested with space debris. This has caused growing concern in recent years, since collisions at orbital velocities can be damaging or dangerous, and can produce more space debris in the process (Kessler Syndrome). The Joint Space Operations Center, part of United States Strategic Command (formerly the United States Space Command), currently tracks more than 8,500 objects larger than 10 cm in LEO, however a limited Arecibo Observatory study suggested there could be approximately one million objects larger than 2 millimeters, which are too small to be visible from Earth.
- List of orbits
- Escape velocity
- Medium Earth Orbit (MEO)
- Highly Elliptical Orbit (HEO)
- Specific orbital energy examples
- International Space Station
- Atmospheric reentry
- Satellite phone
- ^ "IADC Space Debris Mitigation Guidelines" (PDF). Inter-Agency Space Debris Coordination Committee. 15 October 2002. http://www.iadc-online.org/docs_pub/IADC-101502.Mit.Guidelines.pdf.
- ^ "NASA Safety Standard 1740.14, Guidelines and Assessment Procedures for Limiting Orbital Debris" (PDF). Office of Safety and Mission Assurance. 1 August 1995. http://www.orbitaldebris.jsc.nasa.gov/library/NSS1740_14/nss1740_14-1995.pdf.
- ^ "Observing the International Space Station". Canadian Space Agency. http://www.space.gc.ca/asc/eng/educators/resources/observing-student.asp. Retrieved 2008-01-17.
- ^ Fact Sheet: Joint Space Operations Center
- ^ archive of astronomy: space junk
- ^ ISS laser broom, project Orion
Orbits Types General Geocentric About other points Parameters Classical Other Maneuvers
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Look at other dictionaries:
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low Earth orbit — noun A satellite orbit around the Earth within the altitude range of 200 2000 km, in which a satellite can communicate with Earth with a small time lag and energy consumption. Abbreviation: LEO … Wiktionary
low earth orbit — noun Date: 1963 a usually circular orbit from about 90 to 600 miles (about 140 to 970 kilometers) above the earth … New Collegiate Dictionary
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Low Earth Orbit — communication satellite system that orbits the Earth at a low altitude (mainly used for cellular telephone communications), LEO … English contemporary dictionary
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Medium 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… … Wikipedia
Medium 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… … Deutsch Wikipedia