ESA title
Enabling & Support

SOHO operations

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ESA / Enabling & Support / Operations
ROLE Sun observatory
LAUNCH DATE 2 Dec 1995/Atlas II-AS (AC-121)
LAUNCH MASS 1850 kg
ORBIT First Lagrangian point (L1) between the Sun & Earth, 1.5 million km towards the Sun
NOMINAL
MISSION
Approved until December 2009
+ SOHO is conducting the largest- and most-detailed-ever survey of solar surface features +

SOHO is an international collaboration between ESA and NASA. Mission operations are controlled by NASA at Goddard Space Flight Centre, Greenbelt, Maryland. SOHO contributes to the International Solar-Terrestrial Physics Programme, to which ESA, NASA, Japan, Russia, Sweden and Denmark all contribute satellites monitoring the Sun and solar effects.

Information on SOHO mission operations is presented in summary below; links to ESA's main SOHO sites are at right.


The mission

The Solar Heliospheric Observatory (SOHO) is a space-based observatory viewing and investigating the Sun from its deep core through its outer atmosphere - the corona - and the domain of the solar wind, out to a distance ten times beyond the Earth's orbit.

Artist's impression of the SOHO spacecraft
Artist's impression of the SOHO spacecraft

SOHO was built for ESA by Europe's aerospace industry, and is a joint project between ESA and NASA. Of the spacecraft's 12 sets of instruments, nine come from multinational teams led by European scientists, and three from US-led teams.

More than 1500 scientists in 20 countries are directly involved in SOHO's instruments and research programmes. NASA launched SOHO and is responsible for communications and daily operations.


Mission operations overview

SOHO was launched by NASA from Cape Canaveral Air Station, Florida, by an Atlas II-AS (AC-121) rocket, on 2 December 1995.

SOHO mission phases
SOHO mission phases

After a four-month journey the spacecraft reached its vantage point in orbit 1.5 million km nearer to the Sun than the Earth's own orbit. There at the Lagrange Point L1, a point in space where the gravitational pull of the Sun is balanced by the pull of the Earth and the centrifugal force acting on a spacecraft allows it to orbit in step with the Earth.

SOHO can therefore remain hovering around a stable position, relative to the Sun and Earth, in a "halo orbit," while it accompanies the Earth in its annual march around the Sun.

Some of the main tasks of the mission ground controllers are to keep SOHO pointing at the Sun and maintain its halo orbit, which takes it around Lagrange Point L1 roughly every six months. SOHO has an Emergency Sun Reaquisition routine to point it automatically at the Sun in the event of any mishap.


The ground stations

The Canberra Deep Space Communication Complex, Australia
The Canberra Deep Space Communication Complex, Australia

Telemetry and telecommanding are provided by NASA's Deep Space Network, using ground stations located at Goldstone (California), Canberra (Australia) and Madrid (Spain).

Control of the spacecraft was lost in June 1998, and only restored three months later through efforts of the SOHO recovery team. All 12 instruments were still usable, most with no ill effects. Two of the three on-board gyroscopes failed immediately and a third in December 1998. After that, new on-board software that no longer relies on gyroscopes was installed in February 1999. It allowed the spacecraft to return to full scientific operations.


The platform and payload

SOHO's components
SOHO's components

The platform

SOHO was built by industrial companies in 14 European countries, led by Matra-Marconi (now Astrium).

SOHO is a three-axis stabilised spacecraft. The service module, with solar panels, thrusters, attitude control systems, communications and housekeeping functions, was assembled in Toulouse, France. The payload module carrying the scientific instruments was assembled in Portsmouth, UK, and mated with the service module in Toulouse.

The total mass of the spacecraft at launch was 1850 kg. Its length along the sun-pointing axis is 4.3 metres, and the span of the extended solar panels is 9.5 metres.

Payload

Instrument

Name

CDS

Coronal Diagnostic Spectrometer

CELIAS

Charge, Element, and Isotope Analysis System

COSTEP

Comprehensive Suprathermal and Energetic Particle Analyzer

EIT

Extreme ultraviolet Imaging Telescope

ERNE

Energetic and Relativistic Nuclei and Electron experiment

GOLF

Global Oscillations at Low Frequencies

LASCO

Large Angle and Spectrometric Coronagraph

MDI/SOI

Michelson Doppler Imager/Solar Oscillations Investigation

SUMER

Solar Ultraviolet Measurements of Emitted Radiation

SWAN

Solar Wind Anisotropies

UVCS

Ultraviolet Coronagraph Spectrometer

VIRGO

Variability of Solar Irradiance and Gravity Oscillations

For more information on SOHO, access the links at right.

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