Norad Identifikationsnummer: 19162
| Name im Katalog Spacetrack | COSMOS 1932 FUEL CORE |
| Folge COSMOS 1932 FUEL CORE | COSMOS 1932 FUEL CORE Tracker |
| Flugzeiten COSMOS 1932 FUEL CORE | Flugzeiten COSMOS 1932 FUEL CORE |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 14070 |
| Herkunftsland/-organisation | Commonwealth of Independent States (former USSR) (CIS) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Perygeum | 933 km |
| Apogäum | 967 km |
| Neigung der Umlaufbahn (Inklination) | 65.05° |
| Runden pro Tag | 14 |
| Höhe COSMOS 1932 FUEL CORE | 959.48 km |
COSMOS 1932 FUEL CORE, 19162 is a payload satellite owned by VMF (CIS) in LEO that was launched on Mon, 14 Mar 1988 UTC launched from the Tyuratam Missile And Space Complex (TTMTR). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
der Satellit COSMOS 1932 FUEL CORE hinausgetragen 14.03.1988r. Durchschnittshöhe COSMOS 1932 FUEL CORE Text Nummer 1: das. 959.48 km. Durchschnittsgeschwindigkeit COSMOS 1932 FUEL CORE beträgt 26545.6 km/h. Neigung COSMOS 1932 FUEL CORE Satelliten 65.04°.