GLONASS 83, GN 794 - Norad Identifikationsnummer: 28113
| Name im Katalog Spacetrack | COSMOS 2402 (GLONASS) |
| Alternative Bezeichnung | GLONASS 83, GN 794 |
| Gruppe | GLONASS |
| Folge COSMOS 2402 (GLONASS) | COSMOS 2402 (GLONASS) Tracker |
| Folge der Gruppe. GLONASS | Tracker GLONASS |
| Flugzeiten COSMOS 2402 (GLONASS) | Flugzeiten COSMOS 2402 (GLONASS) |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 8320 |
| 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 | 19032 km |
| Apogäum | 19227 km |
| Neigung der Umlaufbahn (Inklination) | 64.33° |
| Runden pro Tag | 2 |
| Höhe COSMOS 2402 (GLONASS) | 19139.07 km |
COSMOS 2402 [GLONASS], also known as Kosmos-2403, is a navigation satellite launched on December 10, 2003, from the TYMSC launch site using LC81/24 and Proton-K/Briz-M as its launch vehicle. The satellite has a bus configuration of Uragan and is 3-Axis stabilized. It measures 4 meters in length with a diameter of 1.5 meters and spans 7.8 meters when fully deployed, including solar arrays. Its dry mass is 1200 kg, and it had an initial launch mass of 1415 kg. The satellite was manufactured by POL (KVR/IACG) for navigation purposes and carries the Uragan No. 95L payload. It uses two deployable solar arrays and batteries for power supply and has a design lifetime of three years. Its shape is described as Cyl + Ant + 2 Pan, with an RCS value of 3.981.
der Satellit COSMOS 2402 (GLONASS) hinausgetragen 10.12.2003r. Durchschnittshöhe COSMOS 2402 (GLONASS) Text Nummer 1: das. 19139.07 km. Durchschnittsgeschwindigkeit COSMOS 2402 (GLONASS) beträgt 14230.59 km/h. Neigung COSMOS 2402 (GLONASS) Satelliten 64.32°.