Akari (satellite)
AKARI (ASTRO-F) was an infrared astronomy satellite developed by Japan Aerospace Exploration Agency, in cooperation with institutes of Europe and Korea. It was launched on 21 February 2006, at 21:28 UTC (06:28, 22 February JST) by M-V rocket into Earth Sun-synchronous orbit. After its launch it was named AKARI (明かり), which means light in Japanese. Earlier on, the project was known as IRIS (InfraRed Imaging Surveyor).
Artist's conception of AKARI | |
Mission type | Infrared telescope |
---|---|
Operator | JAXA |
COSPAR ID | 2006-005A |
SATCAT no. | 28939 |
Website | global |
Mission duration | 5 years, 9 months |
Spacecraft properties | |
Manufacturer | ISAS |
Launch mass | 952 kg (2,099 lb) |
Dimensions | 5.5 m × 1.9 m × 3.2 m (18.0 ft × 6.2 ft × 10.5 ft) |
Start of mission | |
Launch date | 21:28, 21 February 2006 (UTC) |
Rocket | M-V, mission M-V-8 |
Launch site | M-V Pad, Uchinoura Space Center |
End of mission | |
Disposal | decommissioned |
Deactivated | 24 November 2011 |
Decay date | 11 April 2023, 04:44 UTC |
Orbital parameters | |
Reference system | Geocentric |
Regime | Sun-synchronous |
Semi-major axis | 6,884 km (4,278 mi) |
Eccentricity | 0.0129527 |
Perigee altitude | 423.9 km (263.4 mi) |
Apogee altitude | 602.3 km (374.3 mi) |
Inclination | 98.2 degrees |
Period | 94.7 minutes |
RAAN | 305.9392 degrees |
Argument of perigee | 124.2012 degrees |
Mean anomaly | 354.1441 degrees |
Mean motion | 15.1995622 rev/day |
Epoch | 9 July 2015, 13:43:21 UTC |
Revolution no. | 50455 |
Main | |
Type | Ritchey–Chrétien |
Diameter | 0.67 m (2.2 ft) |
Focal length | 4.2 m (14 ft) |
Wavelengths | 1.7 to 180 μm (Infrared) |
Instruments | |
FIS: Far-Infrared Surveyor IRC: Infra-Red Camera | |
Its primary mission was to survey the entire sky in near-, mid- and far-infrared, through its 68.5 cm (27.0 in) aperture telescope.
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