Names | Ямал-202 Yamal-200 KA-2 |
---|---|
Mission type | Communications |
Operator | Gazprom Space Systems |
COSPAR ID | 2003-053A |
SATCAT no. | 28089 |
Website | https://www.gazprom-spacesystems.ru |
Mission duration | 15 years (planned) 20 years, 11 months and 30 days (in progress) |
Spacecraft properties | |
Spacecraft | Yamal-202 |
Spacecraft type | Yamal-200 |
Bus | USP Bus |
Manufacturer | RSC Energia (bus) Alcatel Space (payload) |
Launch mass | 1,320 kg (2,910 lb) |
Power | 3.4 kW |
Start of mission | |
Launch date | 24 November 2003, 06:22:00 UTC |
Rocket | Proton-K / Blok DM-2M |
Launch site | Baikonur, Site 81/23 |
Contractor | Khrunichev State Research and Production Space Center |
Entered service | January 2004 |
Orbital parameters | |
Reference system | Geocentric orbit |
Regime | Geostationary orbit |
Longitude | 49° East (2003-2019) 163.5° East (2019-present) |
Transponders | |
Band | 18 C-band |
Coverage area | Russia |
Yamal-202 (Russian: Ямал-202) is a geostationary communications satellite operated by Gazprom Space Systems and built by RSC Energia.[1] It was, along with Yamal-201 the second dual launch of the Yamal program and the second iteration of the USP Bus.[2][3] It is a 1,320 kg (2,910 lb) satellite with 4,080 watts of power (3.4 kW at end of life) on an unpressurized bus.[4] It has eight SPT-70 electric thrusters by OKB Fakel for station keeping.[5] Its payload is 18 C-band transponders supplied by Space Systems/Loral.[6][7]
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