Globalstar M004 - Norad Identifikationsnummer: 25163
| Name im Katalog Spacetrack | GLOBALSTAR M004 |
| Alternative Bezeichnung | Globalstar M004 |
| Gruppe | GLOBALSTAR |
| Folge GLOBALSTAR M004 | GLOBALSTAR M004 Tracker |
| Folge der Gruppe. GLOBALSTAR | Tracker GLOBALSTAR |
| Flugzeiten GLOBALSTAR M004 | Flugzeiten GLOBALSTAR M004 |
| 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 | 1407 km |
| Apogäum | 1412 km |
| Neigung der Umlaufbahn (Inklination) | 52° |
| Runden pro Tag | 13 |
| Höhe GLOBALSTAR M004 | 1415.35 km |
GLOBALSTAR M004, also known as Globalstar M004, is a communication satellite launched on February 14, 1998, from Cape Canaveral Air Force Station Launch Complex 17A using the Delta 7420-10C launch vehicle. Manufactured by LOR for GLOBT (Globalstar), this spacecraft has dimensions of 1.5 meters in length and a diameter of 0.6 meters with a span of 12 meters due to its deployable solar arrays. The satellites dry mass is 380 kg, and it had a launch mass of 450 kg. It was designed for a communication mission and equipped with batteries alongside the solar arrays for power generation. The spacecraft has a box shape with two panels and an RCS (Reaction Control System) area of 2.2994 square meters. Its operational lifetime was projected to be approximately 7.5 years.
der Satellit GLOBALSTAR M004 hinausgetragen 14.02.1998r. Durchschnittshöhe GLOBALSTAR M004 Text Nummer 1: das. 1415.35 km. Durchschnittsgeschwindigkeit GLOBALSTAR M004 beträgt 25757.72 km/h. Neigung GLOBALSTAR M004 Satelliten 52°.