GLONASS 62, GN 764 - Norad Identifikationsnummer: 23397
| Name im Katalog Spacetrack | COSMOS 2296 (GLONASS) |
| Alternative Bezeichnung | GLONASS 62, GN 764 |
| Gruppe | GLONASS |
| Folge COSMOS 2296 (GLONASS) | COSMOS 2296 (GLONASS) Tracker |
| Folge der Gruppe. GLONASS | Tracker GLONASS |
| Flugzeiten COSMOS 2296 (GLONASS) | Flugzeiten COSMOS 2296 (GLONASS) |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 11627 |
| 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 | 19108 km |
| Apogäum | 19152 km |
| Neigung der Umlaufbahn (Inklination) | 64.9° |
| Runden pro Tag | 2 |
| Höhe COSMOS 2296 (GLONASS) | 19139.04 km |
The COSMOS 2296 [GLONASS] satellite, also known as Kosmos-2295, is a navigation satellite belonging to the Russian military (VKS). Launched on November 20, 1994, from the TYMSC launch site using the Proton-K/DM-2 vehicle, it was manufactured by POL and has a configuration of 3-axis stabilization. The satellite carries the Uragan No. 63L payload for navigation purposes. It measures 4 meters in length with a diameter of 1.5 meters and a span of 7.8 meters when its solar arrays are deployed. At launch, it had a mass of 1300 kg and a dry mass of 1200 kg. The power system consists of two deployable solar arrays and batteries. Its shape is described as cylindrical with antennas and panels. The satellites design lifetime was estimated to be three years.
der Satellit COSMOS 2296 (GLONASS) hinausgetragen 20.11.1994r. Durchschnittshöhe COSMOS 2296 (GLONASS) Text Nummer 1: das. 19139.04 km. Durchschnittsgeschwindigkeit COSMOS 2296 (GLONASS) beträgt 14230.66 km/h. Neigung COSMOS 2296 (GLONASS) Satelliten 64.89°.