High Earth orbit

Source: Wikipedia, the free encyclopedia.
This article is about a type of geocentric orbit defined by altitude. For a more common disambiguation of HEO, see Highly elliptical orbit.
Space of high Earth orbits (HEO), between medium Earth orbits (MEO) and the orbit of the Moon.

A high Earth orbit is a geocentric orbit with an apogee farther than that of the geosynchronous orbit, which is 35,786 km (22,236 mi) away from Earth.[1] In this article, the non-standard abbreviation of HEO is used for high Earth orbit.[2]

The development of HEO technology has had a significant impact on space exploration and has paved the way for future missions to deep space. The ability to place satellites in HEO has allowed scientists to make groundbreaking discoveries in astronomy and Earth science, while also enabling global communication and navigation systems.[3]

The Moon's Hill sphere is entered at a distance to the Moon of 60,000 km (37,000 mi),[4] lunar orbits until a distance of 690 km (430 mi) are unstable due to Earth's gravitational reach.[5]

cislunar space
. Earth's hill sphere extends to a distance of 1,471,400 km (914,300 mi), encompassing
interplanetary space
.

Common types of high Earth orbits

A view of a crescent Earth taken from inside Apollo 13’s Lunar Module on 17 April 1970. Credit: NASA / restored by Toby Ord
Orbit Name
GEO Geostationary orbit
GSO Geosynchronous orbit
GTO Geostationary transfer orbit
HEO Highly elliptical orbit
NRHO Near-rectilinear halo orbit

Satellites in High Earth orbits are primarily used for

military applications.[6]
One of the main benefits of HEO is that it provides a nearly unobstructed view of the Earth and deep space. This makes it an ideal location for astronomical observations and Earth monitoring. In addition, satellites in HEO can provide a continuous coverage of the Earth's surface, making it very useful for communication and navigation purposes.
TESS,[8]
have been placed in HEO.

There are four main reasons that most satellite are placed in lower orbits. First, a HEO can take a month or more per orbit. This is because HEOs are very large orbits and move at only 7000 mph. Meanwhile, a

shielding
to protect them from radiation. As a result, only satellites that require the unique characteristics of HEO use this orbit.

A special case of a high Earth orbit is the highly elliptical orbit where altitude at perigee may reach as low as 2,000 km (1,200 mi).

Examples of satellites in high Earth orbit

Name NSSDC id. Launch date Perigee Apogee Period Inclination
Vela 1A[11][12] 1963-039A 1963-10-17 101,925 km 116,528 km 108 hr 39 min 37.8°
IBEX 2008-051A 2008-10-19 61,941 km 290,906 km 216 hr 3 min 16.9°
TESS[8][13]
 2018-038A 2018-04-18 108,000 km 375,000 km 328 hr 48 min 37.00°
Chdryn.-3 prop. module 2023-098B 2023-07-14 115,000 km 154,000 km ~312 hr 27°

See also

References

  1. ^ "Catalog of Earth Satellite Orbits". earthobservatory.nasa.gov. NASA Earth Observatory. 2009-09-04. p. 1. Retrieved 2023-04-05.
  2. ^ "Types of Orbits". spacefoundation.org. Space Foundation. Retrieved 2023-04-22.
  3. ^ "Catalog of Earth Satellite Orbits: Three Classes of Orbit". earthobservatory.nasa.gov. NASA Earth Observatory. 2009-09-04. p. 2. Retrieved 2023-04-05.
  4. NASA.gov
    . Greenbelt, MD: NASA Goddard Space Flight Center. Retrieved 23 July 2023.
  5. ^ "A New Paradigm for Lunar Orbits". Phys.org. 2006-12-01. Retrieved 2023-11-05.
  6. ^ "Types of Orbits". spacefoundation.org. Retrieved April 22, 2023.
  7. ^ "Advantages of HEO Highly Elliptical Orbit | Disadvantages of HEO orbit".
  8. ^ a b "MIT TESS mission". Retrieved November 12, 2022.
  9. ^ "Popular Orbits 101". Aerospace Security. 30 November 2017. Retrieved 2023-04-05.
  10. ^ "Capabilities & Services" (PDF). spacex.com. Retrieved April 22, 2023.
  11. ^ "Vela". Astronautix.com. Retrieved November 12, 2022.
  12. ^ "Trajectory Details for Vela 1A from the National Space Science Data Center". Retrieved November 12, 2022.
  13. ^ "NASA - TESS Science Support Center". 25 July 2023.
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