GLOBALSTAR M004
Satellite information GLOBALSTAR M004 - Globalstar M004
| Spacetrack Directory Name | GLOBALSTAR M004 |
| Alternative name | Globalstar M004 |
| Group | GLOBALSTAR |
| Follow GLOBALSTAR M004 | GLOBALSTAR M004 Tracker |
| Group follow GLOBALSTAR | Tracker GLOBALSTAR |
| Pass predictions GLOBALSTAR M004 | Pass predictions GLOBALSTAR M004 |
| 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 | 1407 km |
| Apogee | 1412 km |
| Orbit slope (inclination) | 52° |
| Laps per day | 13 |
| Height GLOBALSTAR M004 | 1415.35 km |
Additional information GLOBALSTAR M004
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.
satellite GLOBALSTAR M004 Date of exalting 14.02.1998y. Average height of ISS GLOBALSTAR M004 hundred 1415.35 km. Average velocity GLOBALSTAR M004 is 25757.72 km/h. Inclination GLOBALSTAR M004 satellite 52°.TLE
Average velocity GLOBALSTAR M004
Average inclination GLOBALSTAR M004
Mean right ascension of the ascending node (RAAN) GLOBALSTAR M004
Mean argument of perigee GLOBALSTAR M004
Mean semi-major axis of the orbit GLOBALSTAR M004
Mean orbital eccentricity GLOBALSTAR M004
ISS
Buy us a coffee!
