Ekspress-MD1

Ekspress-MD1
NamesЭкспресс-МД1
Express-MD1
Mission typeCommunications
OperatorRussian Satellite Communications Company (RSCC)
COSPAR ID2009-007B
SATCAT no.33596
Websitehttps://eng.rscc.ru/
Mission duration10 years (planned)
4.3 years (achieved)
Spacecraft properties
SpacecraftEkspress-MD1
Spacecraft typeEkspress-MD
BusYakhta modified
ManufacturerKhrunichev (bus)
Alcatel Alenia Space (payload)
Launch mass1,140 kg (2,510 lb)
Power1300 watts
Start of mission
Launch date11 February 2009, 00:03:00 UTC
RocketProton-M / Briz-M
Launch siteBaikonur, Site 200/39
ContractorKhrunichev State Research and Production Space Center
Entered service12 May 2009
End of mission
DisposalFailed on orbit
Last contact4 July 2013
Orbital parameters
Reference systemGeocentric orbit
RegimeGeostationary orbit
Longitude80° East
Transponders
Band8 × 40 Mhz C-band
1 × 1 MHz L-band
Bandwidth321 MHz
Coverage areaRussia, CIS

Ekspress-MD1 (Russian: Экспресс-МД1), was a Russian geostationary communications satellite operated by Russian Satellite Communications Company (RSCC) and designed and manufactured by Khrunichev State Research and Production Space Center on the Yakhta satellite bus for RSCC's Ekspress series. It massed 1,140 kg (2,510 lb) at launch, had a power production capacity of 1300 watts with a C-band and L-band payload.

It was successfully launched along Ekspress-AM4 aboard a Proton-M / Briz-M from Baikonur on 11 February 2009. It was commissioned in the 80° East orbital position. The satellite failed on 4 July 2013, well short of its design life, for which RSCC collected the insurance.