Globalstar M001 - Norad Identifikationsnummer: 25162
| Name im Katalog Spacetrack | GLOBALSTAR M001 |
| Alternative Bezeichnung | Globalstar M001 |
| Gruppe | GLOBALSTAR |
| Folge GLOBALSTAR M001 | GLOBALSTAR M001 Tracker |
| Folge der Gruppe. GLOBALSTAR | Tracker GLOBALSTAR |
| Flugzeiten GLOBALSTAR M001 | Flugzeiten GLOBALSTAR M001 |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 10432 |
| Herkunftsland/-organisation | Globalstar (GLOB) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Typ | Satellit |
| Kategorie | |
| Perygeum | 1513 km |
| Apogäum | 1516 km |
| Neigung der Umlaufbahn (Inklination) | 52° |
| Runden pro Tag | 12 |
| Höhe GLOBALSTAR M001 | 1520.58 km |
GLOBALSTAR M001 (NORAD_CAT_ID: 25162) is a communication satellite owned by GLOBT and manufactured by LOR. It was launched on February 14, 1998, from Cape Canaveral Air Force Stations LC17A using the Delta 7420-10C launch vehicle. The satellite has dimensions of 1.5 meters in length and 0.6 meters in diameter with a span of 12 meters, indicating deployable components such as solar arrays. Its dry mass is 380 kilograms and its total launch mass was 450 kilograms. It is equipped with two deployable solar arrays and batteries for power supply. The satellites shape is described as Box + 2 Pan and has a radar cross-section (RCS) of 1.807 square meters. Its operational lifetime was expected to be around 7.5 years, dedicated to communication purposes.
der Satellit GLOBALSTAR M001 hinausgetragen 14.02.1998r. Durchschnittshöhe GLOBALSTAR M001 Text Nummer 1: das. 1520.58 km. Durchschnittsgeschwindigkeit GLOBALSTAR M001 beträgt 25585.4 km/h. Neigung GLOBALSTAR M001 Satelliten 52°.