Technical Information
NileSat 101 was launched on the Ariane 4, manufactured by the European company Matra Marconi Space (Astrium) Nilesat 101 has been launched in April 1998 . has life time of 15 years. Each carries 12 Ku-band transponders of 33 MHz bandwidth to provide digital communications and terrestrial Direct-to-Home TV, Radio Broadcasting, Multimedia and Data services for countries in North Africa, South Europe and the Middle East.
|
Launch Information
|
| Launch Date |
|
| Launch Vehicle |
|
| Launch Mass |
|
| Orbital Information |
| Satellite Manufacturer |
|
| Orbital Position |
|
| Stabilization System |
|
| Station Keeping Co-location Accuracy |
|
| System Power Consumption (Max) |
|
| Expected Life Time |
|
| Payload Information |
| EIRP (Max.) |
|
| G/T (Max.) |
|
| Downlink Frequency Band (KU) |
|
| Uplink Frequency Band (KU) |
|
| Transponder Bandwidth |
|
| Transponder Output Power |
|
| TWTA Redundancy |
|
| Polarization |
|
| aturation Flux Density (FGM) *london Horn |
|
| Transponder Gain Range |
|
| Operation Information |
| Receiving Dish Diameter |
|
| Operation Start Date |
|