SES 12
Informationen über den Satelliten. SES 12 - SES-12
| Name im Katalog Spacetrack | SES 12 |
| Alternative Bezeichnung | SES-12 |
| Gruppe | SES |
| Folge SES 12 | SES 12 Tracker |
| Folge der Gruppe. SES | Tracker SES |
| Flugzeiten SES 12 | Flugzeiten SES 12 |
| In die Umlaufbahn bringen |
2018-06-04 (8 vor Jahren)
|
| Tage im Orbit | 3077 |
| 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 | 35777 km |
| Apogäum | 35797 km |
| Neigung der Umlaufbahn (Inklination) | 0.02° |
| Runden pro Tag | 1 |
| Orbit | GEO |
| Höhe SES 12 | 35786.46 km |
Informationen über SES 12
SES-12 is a communication satellite, also known by its alternate name SES-12, operated by SESSA. It was manufactured by ADST and uses the Eurostar 3000e bus configuration. The satellite has dimensions of 5.4 meters in length, 3 meters in diameter, and spans 39.3 meters when fully deployed. It has a dry mass of 3000 kilograms and a launch mass of 5384 kilograms, equipped with power from two deployable solar arrays and batteries.
SES-12 was launched on June 4, 2018, from the Cape Canaveral Air Force Stations Launch Complex 40 using a Falcon 9 launch vehicle. Its equipment includes 68 active Ku-band transponders and 8 Ka-band transponders for communication purposes. The satellite is designed to operate for an estimated lifetime of 18 years.
The spacecraft has a box shape with two solar panel arrays (Pan) and its primary mission is to provide communication services. It was built in Luxembourg (L) and its motor type is EOR.
Orbital Elemente
Durchschnittsgeschwindigkeit SES 12
Durchschnitt SES 12
Mittlere Rektaszension des aufsteigenden Knotens (RAAN) SES 12
Mittleres Argument des Perigäums SES 12
Mittlere große Halbachse der Umlaufbahn SES 12
Mittlere Bahnexzentrizität SES 12
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