GLONASS-M 8, GN 715 - Norad Identifikationsnummer: 29672
| Name im Katalog Spacetrack | COSMOS 2424 (GLONASS) |
| Alternative Bezeichnung | GLONASS-M 8, GN 715 |
| Gruppe | GLONASS |
| Folge COSMOS 2424 (GLONASS) | COSMOS 2424 (GLONASS) Tracker |
| Folge der Gruppe. GLONASS | Tracker GLONASS |
| Flugzeiten COSMOS 2424 (GLONASS) | Flugzeiten COSMOS 2424 (GLONASS) |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 7209 |
| Herkunftsland/-organisation | Commonwealth of Independent States (former USSR) (CIS) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Typ | Satellit |
| Kategorie | |
| Perygeum | 19081 km |
| Apogäum | 19175 km |
| Neigung der Umlaufbahn (Inklination) | 64.7° |
| Runden pro Tag | 2 |
| Orbit | MEO (Nicht-polar geneigt) |
| Höhe COSMOS 2424 (GLONASS) | 19137.15 km |
The COSMOS 2424 [GLONASS-M], also known as Kosmos-2426, is a navigation satellite launched on December 25, 2006, from the TYMSC launch site using a Proton-K/DM-2 launch vehicle. With dimensions of 4 meters in length and 1.5 meters in diameter, it has a span of 7.8 meters when its solar arrays are deployed. The satellite carries a dry mass of 1200 kg and had a launch mass of 1450 kg. It is based on the 3-Axis stabilized Uragan-M bus design and was manufactured by RESH for KVR/IACG. Its mission is to provide navigation services as part of the GLONASS constellation, with its operational lifetime planned for seven years. The satellites power system includes two deployable solar arrays and batteries.
der Satellit COSMOS 2424 (GLONASS) hinausgetragen 25.12.2006r. Durchschnittshöhe COSMOS 2424 (GLONASS) Text Nummer 1: das. 19137.15 km. Durchschnittsgeschwindigkeit COSMOS 2424 (GLONASS) beträgt 14231.19 km/h. Neigung COSMOS 2424 (GLONASS) Satelliten 64.7°.