COSMOS 2084
Informationen über den Satelliten. COSMOS 2084
| Name im Katalog Spacetrack | COSMOS 2084 |
| Folge COSMOS 2084 | COSMOS 2084 Tracker |
| Flugzeiten COSMOS 2084 | Flugzeiten COSMOS 2084 |
| In die Umlaufbahn bringen |
1990-06-21 (36 vor Jahren)
|
| Tage im Orbit | 13240 |
| Herkunftsland/-organisation | Commonwealth of Independent States (former USSR) (CIS) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | PLMSC (Plesetsk Missile and Space Complex, Russia) |
| Kategorie | |
| Perygeum | 561 km |
| Apogäum | 622 km |
| Neigung der Umlaufbahn (Inklination) | 62.79° |
| Runden pro Tag | 15 |
| Höhe COSMOS 2084 | 556.36 km |
Informationen über COSMOS 2084
Kosmos 2084 (Russian: ?????? 2084 meaning Cosmos 2084) is a Russian US-K missile early warning satellite which was launched in 1990 as part of the Russian Space Forces' Oko programme. The satellite was designed to identify missile launches using optical telescopes and infrared sensors.Kosmos 2084 was launched from Site 43/3 at Plesetsk Cosmodrome in Russia. A Molniya-M carrier rocket with a 2BL upper stage was used to perform the launch, which took place at 20:45 UTC on 21 June 1990. The launch failed to place the satellite into a molniya orbit as the Blok 2BL failed to ignite leaving the satellite in low Earth orbit.
It subsequently received its Kosmos designation, and the international designator 1990-055A. The United States Space Command assigned it the Satellite Catalog Number 20663.
Orbital Elemente
Durchschnittshöhe der Orbitalbahn. COSMOS 2084
Durchschnittsgeschwindigkeit COSMOS 2084
Durchschnitt COSMOS 2084
Mittlere Rektaszension des aufsteigenden Knotens (RAAN) COSMOS 2084
Mittleres Argument des Perigäums COSMOS 2084
Mittlere große Halbachse der Umlaufbahn COSMOS 2084
Mittlere Bahnexzentrizität COSMOS 2084
Internationale Raumstation
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