Astra 1L : As suas caracteristicas

Preliminary Footprint : FSS beam

Satellite construction information:

Construction: June 2003 - March 2007
in Newton (PHL) and Sunnyvale (San Francisco)
Transport to Kourou: by a Russian Antonov Cargo plane from Sunnyvale to Kourou

Satellite launch information:
Launch date:04.05.2007
Launch vehicle:Ariane V ECA
Launch site:Kourou, French Guiana
Launch mass: 4500 kg

Satellite orbital information:
Satellite manufacturer: Lockheed Martin
Satellite type: A2100 AX
Orbital location: 19.2 degrees East Longitude
Stabilization system: 3-axis type
Total power consumption: 13,074 W

Satellite transponder information:
Transponder capacity: 25 Ku + 2 Ka End of Life
29 Ku + 2 Ka First Five Years
TWTA output power:140 W (Ku Band)
128 W (Ka Band)
EIRP: 46 to 54.5 dBW

All transponders are eclipse protected
Transponder bandwidth:
26 MHz (Bands A,B,C and G)
33 MHz (Band F)
500 MHz (Ka Band)

Channel capacity:

10.7-12.75 GHz:72 Ku band channels
(Bands A, B, C, F, G)

Fonte: ses-astra