SES-11 (ECHOSTAR 105) - Norad Identifikationsnummer: 42967
| Name im Katalog Spacetrack | ECHOSTAR 105/SES 11 |
| Alternative Bezeichnung | SES-11 (ECHOSTAR 105) |
| Gruppe | SES |
| Folge ECHOSTAR 105/SES 11 | ECHOSTAR 105/SES 11 Tracker |
| Folge der Gruppe. SES | Tracker SES |
| Flugzeiten ECHOSTAR 105/SES 11 | Flugzeiten ECHOSTAR 105/SES 11 |
| In die Umlaufbahn bringen |
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| Tage im Orbit | 3267 |
| Herkunftsland/-organisation | SES |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Typ | Satellit |
| WWW | hier |
| Kategorie | |
| Perygeum | 35776 km |
| Apogäum | 35798 km |
| Neigung der Umlaufbahn (Inklination) | 0.04° |
| Runden pro Tag | 1 |
| Orbit | GEO |
| Höhe ECHOSTAR 105/SES 11 | 35786.13 km |
SES-11 (ECHOSTAR 105) is a communication satellite, also known by its alternate name SES-11. Launched on October 11, 2017, from the Air Force Eastern Test Range Launch Complex 39A using a Falcon 9 launch vehicle, it has a configuration based on the Eurostar-3000 bus manufactured by ADSB. The satellite is owned and operated by SESSA (SES S.A.) and carries a payload that includes 24 Ku-band transponders and 24 C-band transponders for communication purposes.
With dimensions of 7 meters in length, 3.3 meters in diameter, and a span of 35 meters due to its solar arrays, SES-11 has a dry mass of 3000 kilograms and was launched with a total mass of 5300 kilograms. It is equipped with two deployable solar arrays for power generation along with batteries. The satellites design features a box shape with two panels and it uses R-4D-15 motors as propulsion systems. Its expected operational lifetime is 15 years, fulfilling its mission to provide communication services.