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Solar and Heliospheric Observatory

Solar and Heliospheric Observatory (SOHO)
NASA SOHO spacecraft.png
Artist's concept of SOHO
Mission type Solar observation
Operator ESA / NASA
COSPAR ID 1995-065A
SATCAT no. 23726
Website sohowww.nascom.nasa.gov
Mission duration 3 years planned
21 years, 3 months and 9 days elapsed
Spacecraft properties
Manufacturer Matra Marconi Space
Launch mass 1,850 kg (4,080 lb)
Payload mass 610 kg (1,340 lb)
Dimensions 4.3 m × 2.7 m × 3.7 m (14.1 ft × 8.9 ft × 12.1 ft)
Power 1500 watts
Start of mission
Launch date 08:08:ss, December 2, 1995 (1995-12-02T08:08:ss)
Rocket Atlas IIAS AC-121
Launch site Cape Canaveral LC-36B
Orbital parameters
Reference system Sun–Earth L1
Regime Halo orbit
Periapsis 206,448 km (128,281 mi)
Apoapsis 668,672 km (415,494 mi)
Epoch planned

SOHO mission insignia
ESA solar system insignia for the SOHO mission

Cluster →

SOHO mission insignia
ESA solar system insignia for the SOHO mission

The Solar and Heliospheric Observatory (SOHO) is a spacecraft built by a European industrial consortium led by Matra Marconi Space (now Astrium) that was launched on a Lockheed Martin Atlas II AS launch vehicle on December 2, 1995 to study the Sun, and has discovered over 3000 comets. It began normal operations in May 1996. It is a joint project of international cooperation between the European Space Agency (ESA) and NASA. Originally planned as a two-year mission, SOHO continues to operate after over 20 years in space. In June 2013, a mission extension lasting until December 2016 was approved.

In addition to its scientific mission, it is the main source of near-real-time solar data for space weather prediction. Along with the GGS Wind, Advanced Composition Explorer (ACE) and DSCOVR, SOHO is one of four spacecraft in the vicinity of the EarthSun L1 point, a point of gravitational balance located approximately 0.99 astronomical unit (AU)s from the Sun and 0.01 AU from the Earth. In addition to its scientific contributions, SOHO is distinguished by being the first three-axis-stabilized spacecraft to use its reaction wheels as a kind of virtual gyroscope; the technique was adopted after an on-board emergency in 1998 that nearly resulted in the loss of the spacecraft.


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