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**HYLAS 2**
Spacecraft properties

Mission type	Communication
Operator	Avanti Communications
COSPAR ID	2012-043B
SATCAT no.	38741
Mission duration	15 years


Bus	STAR-2
Manufacturer	Orbital Sciences Corporation
Launch mass	3,325 kilograms (7,330 lb)
Power	5 KW


Start of mission
Launch date	2 August 2012 (2012-08-02)
Rocket	Ariane 5ECA
Launch site	Kourou ELA-3
Contractor	Arianespace


Orbital parameters
Reference system	Geocentric
Regime	Geostationary
Longitude	31.0° East


Transponders
Band	24 + 6 K_a band (NATO K band)

HYLAS 2 is a geostationary High throughput satellite operated by Avanti Communications. HYLAS, an acronym for Highly Adaptable Satellite, was launched on Ariane 5 from Guyana Space Centre at Kourou, French Guiana, on 2 August 2012.

Construction

HYLAS 2 was constructed by Orbital Sciences Corporation on the STAR-2 platform for the UK telecommunications company Avanti Communications Plc.

Features

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.

References

"HYLAS2" (PDF).
"HYLAS 2 Product Sheet" (PDF). datasheet. Avanti Communications Group plc. 10 August 2012. Archived from the original (PDF) on 10 August 2013. Retrieved 3 November 2012.
Freedomsat - HYLAS 2 Coverage Archived 2012-10-23 at the Wayback Machine
- Hylas-2 Internet Coverage

v t e ← 2011 Orbital launches in 2012 2013 →
January	Ziyuan III-01, VesselSat-2 Fengyun 2-07 USA-233 Progress M-14M
February	Navid LARES, ALMASat-1, Xatcobeo, UniCubeSat-GG, ROBUSTA, e-st@r, Goliat, MaSat-1, PW-Sat SES-4 Compass-G5 MUOS-1
March	Edoardo Amaldi ATV Intelsat 22 Kosmos 2479 Apstar 7
April	USA-234 Kwangmyŏngsŏng-3 Progress M-15M YahSat-1B RISAT-1 Compass-M3, Compass-M4
May	USA-235 Tianhui 1B Yaogan 14, Tiantuo 1 Soyuz TMA-04M JCSAT-13, Vinasat-2 Kosmos 2480 Shizuku, Kompsat 3, SDS-4, Horyu 2 Nimiq 6 SpaceX COTS Demo Flight 2, New Frontier Fajr ChinaSat 2A Yaogan 15
June	Intelsat 19 NuSTAR Shenzhou 9 USA-236 / Quasar 18 USA-237 / Orion 8
July	EchoStar XVII, MSG-3 SES-5 Soyuz TMA-05M Kounotori 3 (Raiko, We-Wish, Niwaka, TechEdSat, F-1) Kanopus-V1, BelKA-2, Zond-PP, TET-1, exactView-1 Tianlian I-03 Gonets-M No.3, Gonets-M No.4, Kosmos 2481, MiR
August	Progress M-16M (Sfera-53) Intelsat 20, HYLAS 2 Telkom-3, Ekspress-MD2 Intelsat 21 RBSP-A, RBSP-B
September	SPOT 6, PROITERES, mRESINS USA-238, SMDC-ONE 1.1, SMDC-ONE 1.2, AeroCube 4, AeroCube 4A, AeroCube 4B, Aeneas, Re, CSSWE, CP5, CXBN, CINEMA 1 MetOp-B Compass-M5, Compass-M6 Astra 2F, GSAT-10 VRSS-1
October	USA-239 SpaceX CRS-1, Orbcomm-2 David, Sif Shijian 9-01, Shijian 9-02 Intelsat 23 Soyuz TMA-06M Compass G6 Progress M-17M
November	Luch 5B, Yamal-300K Eutelsat 21B, Star One C3 Meridian 6 Huanjing 1C EchoStar XVI Yaogan 16A, Yaogan 16B, Yaogan 16C ChinaSat 12
December	Pléiades-HR 1B Eutelsat 70B Yamal-402 USA-240 Kwangmyŏngsŏng-3 Unit 2 Göktürk-2 Soyuz TMA-07M Skynet 5D, Mexsat Bicentenario
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ). Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).

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Categories:

Construction

Features

See also

References