EXOSAT
| EXOSAT | |
| Mission type | Astronomy | 
|---|---|
| Operator | ESA | 
| COSPAR ID | 1983-051A | 
| SATCAT no. | 14095 | 
| Website | www | 
| Mission duration | 3 years | 
| Spacecraft properties | |
| Manufacturer | MBB | 
| Launch mass | 510.0 kg (1,124.4 lb) | 
| Power | 165.0 watts | 
| Start of mission | |
| Launch date | 26 May 1983, 15:18:00 UTC | 
| Rocket | Delta 3914 D169 | 
| Launch site | Vandenberg SLC-2W | 
| End of mission | |
| Decay date | 5 May 1986 | 
| Orbital parameters | |
| Reference system | Geocentric | 
| Regime | Low Earth | 
| Eccentricity | 0.93428 | 
| Perigee altitude | 347 km (216 mi) | 
| Apogee altitude | 191,709 km (119,122 mi) | 
| Inclination | 72.5 degrees | 
| Period | 5,435.4 minutes | 
| Epoch | 26 May 1983, 11:18:00 UTC | 
| Legacy ESA insignia for the EXOSAT mission | |
The European X-ray Observatory Satellite (EXOSAT), originally named HELOS, was an X-ray telescope operational from May 1983 until April 1986 and in that time made 1780 observations in the X-ray band of most classes of astronomical object including active galactic nuclei, stellar coronae, cataclysmic variables, white dwarfs, X-ray binaries, clusters of galaxies, and supernova remnants.
This European Space Agency (ESA) satellite for direct-pointing and lunar-occultation observation of X-ray sources beyond the Solar System was launched into a highly eccentric orbit (apogee 200,000 km, perigee 500 km) almost perpendicular to that of the Moon on 26 May 1983. The instrumentation includes two low-energy imaging telescopes (LEIT) with Wolter I X-ray optics (for the 0.04–2 keV energy range), a medium-energy experiment using Ar/CO2 and Xe/CO2 detectors (for 1.5–50 keV), a Xe/He gas scintillation spectrometer (GSPC) (covering 2–80 keV), and a reprogrammable onboard data-processing computer. Exosat was capable of observing an object (in the direct-pointing mode) for up to 80 hours and of locating sources to within at least 10 arcsec with the LEIT and about 2 arcsec with GSPC.