GLOBALSTAR M001
Satellite information GLOBALSTAR M001 - Globalstar M001
| Spacetrack Directory Name | GLOBALSTAR M001 |
| Alternative name | Globalstar M001 |
| Group | GLOBALSTAR |
| Follow GLOBALSTAR M001 | GLOBALSTAR M001 Tracker |
| Group follow GLOBALSTAR | Tracker GLOBALSTAR |
| Pass predictions GLOBALSTAR M001 | Pass predictions GLOBALSTAR M001 |
| Orbit launches |
1998-02-14 (28 years ago)
|
| Days in orbit | 10432 |
| Country/organisation of origin | Globalstar (GLOB) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Type | Satellite |
| Categories | |
| Perigee | 1513 km |
| Apogee | 1516 km |
| Orbit slope (inclination) | 52° |
| Laps per day | 12 |
| Height GLOBALSTAR M001 | 1520.58 km |
Additional information GLOBALSTAR M001
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.
satellite GLOBALSTAR M001 Date of exalting 14.02.1998y. Average height of ISS GLOBALSTAR M001 hundred 1520.58 km. Average velocity GLOBALSTAR M001 is 25585.4 km/h. Inclination GLOBALSTAR M001 satellite 52°.TLE
Average velocity GLOBALSTAR M001
Average inclination GLOBALSTAR M001
Mean right ascension of the ascending node (RAAN) GLOBALSTAR M001
Mean argument of perigee GLOBALSTAR M001
Mean semi-major axis of the orbit GLOBALSTAR M001
Mean orbital eccentricity GLOBALSTAR M001
ISS
Buy us a coffee!
