This articleneeds additional citations forverification. Please helpimprove this article byadding citations to reliable sources. Unsourced material may be challenged and removed. Find sources: "HYLAS 2" – news ·newspapers ·books ·scholar ·JSTOR(September 2012) (Learn how and when to remove this message) |
Mission type | Communication[1] |
---|---|
Operator | Avanti Communications |
COSPAR ID | 2012-043B![]() |
SATCATno. | 38741![]() |
Mission duration | 15 years |
Spacecraft properties | |
Bus | STAR-2 |
Manufacturer | Orbital Sciences Corporation |
Launch mass | 3,325 kilograms (7,330 lb) |
Power | 5 KW[2] |
Start of mission | |
Launch date | 2 August 2012 (2012-08-02) |
Rocket | Ariane 5ECA |
Launch site | KourouELA-3 |
Contractor | Arianespace |
Orbital parameters | |
Reference system | Geocentric |
Regime | Geostationary |
Longitude | 31.0° East |
Transponders | |
Band | 24 + 6Ka band (NATOK band) |
HYLAS 2 is ageostationaryHigh throughput satellite operated byAvanti Communications. HYLAS, an acronym forHighly Adaptable Satellite, was launched onAriane 5 fromGuyana Space Centre atKourou,French Guiana, on 2 August 2012.
HYLAS 2 was constructed byOrbital Sciences Corporation on theSTAR-2 platform for the UK telecommunications company Avanti Communications Plc.
HYLAS 2 features 4 active and 6 gateway Ka beams covering Northern and Southern Africa, Eastern Europe and the Middle East. HYLAS 2 is also equipped with steerable spot-beams to direct extra capacity in required areas when needed.[3][4]
![]() | This article about one or morecommunications satellites is astub. You can help Wikipedia byexpanding it. |