INTELSAT 35E (IS-35E) - Norad Identifikationsnummer: 42818
| Name im Katalog Spacetrack | INTELSAT 35E |
| Alternative Bezeichnung | INTELSAT 35E (IS-35E) |
| Gruppe | INTELSAT |
| Folge INTELSAT 35E | INTELSAT 35E Tracker |
| Folge der Gruppe. INTELSAT | Tracker INTELSAT |
| Flugzeiten INTELSAT 35E | Flugzeiten INTELSAT 35E |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 3365 |
| Herkunftsland/-organisation | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Typ | Satellit |
| Kategorie | |
| Perygeum | 35778 km |
| Apogäum | 35795 km |
| Neigung der Umlaufbahn (Inklination) | 0.02° |
| Runden pro Tag | 1 |
| Orbit | GEO |
| Höhe INTELSAT 35E | 35786.42 km |
INTELSAT 35E (IS-35E) is a communication satellite owned by INTELU and was launched on July 5, 2017, from LC39A at AFETR using a Falcon 9 launch vehicle. It has dimensions of 7.5 meters in length, 3 meters in diameter, and spans 44 meters with its solar arrays deployed. The satellites dry mass is 3500 kg, and it was launched with a total mass of 6761 kg. Equipped with C-band and Ku-band high-throughput transponders for communication purposes, IS-35E is powered by two deployable solar arrays and batteries. It operates on a BSS-702MP bus manufactured by BOES and features an IHI BT-4 motor. The satellites shape includes a box with two panels and its intended lifetime is 15 years.
der Satellit INTELSAT 35E hinausgetragen 05.07.2017r. Durchschnittshöhe INTELSAT 35E Text Nummer 1: das. 35786.42 km. Durchschnittsgeschwindigkeit INTELSAT 35E beträgt 11068.94 km/h. Neigung INTELSAT 35E Satelliten 0.02°.