GLOBALSTAR M060
Satellite information GLOBALSTAR M060 - Globalstar M060
| Spacetrack Directory Name | GLOBALSTAR M060 |
| Alternative name | Globalstar M060 |
| Group | GLOBALSTAR |
| Follow GLOBALSTAR M060 | GLOBALSTAR M060 Tracker |
| Group follow GLOBALSTAR | Tracker GLOBALSTAR |
| Pass predictions GLOBALSTAR M060 | Pass predictions GLOBALSTAR M060 |
| Orbit launches |
2000-02-08 (26 years ago)
|
| Days in orbit | 9705 |
| Country/organisation of origin | Globalstar (GLOB) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Type | Satellite |
| WWW | Here |
| Categories | |
| Perigee | 1600 km |
| Apogee | 1606 km |
| Orbit slope (inclination) | 52° |
| Laps per day | 12 |
| Height GLOBALSTAR M060 | 1609.33 km |
Additional information GLOBALSTAR M060
GLOBALSTAR M060, also known as Globalstar M060, is a communication satellite launched on February 8, 2000, from Cape Canaveral Air Force Stations SLC17B launch pad using the Delta 7420-10C launch vehicle. The spacecraft measures 1.5 meters in length and has a diameter of 0.6 meters with a span of 12 meters when deployed. It weighs 380 kilograms dry and had an initial launch mass of 450 kilograms. Manufactured by LOR, the satellite uses the LS-400 AOCS motor for its attitude control system and is powered by two deployable solar arrays and batteries. The mission of GLOBALSTAR M060 involves communication purposes with a specified lifetime of 7.5 years. It was owned by GLOBT and carries the payload Globalstar FM60, featuring a box shape with two panels.
satellite GLOBALSTAR M060 Date of exalting 08.02.2000y. Average height of ISS GLOBALSTAR M060 hundred 1609.33 km. Average velocity GLOBALSTAR M060 is 25442.84 km/h. Inclination GLOBALSTAR M060 satellite 52°.TLE
Average velocity GLOBALSTAR M060
Average inclination GLOBALSTAR M060
Mean right ascension of the ascending node (RAAN) GLOBALSTAR M060
Mean argument of perigee GLOBALSTAR M060
Mean semi-major axis of the orbit GLOBALSTAR M060
Mean orbital eccentricity GLOBALSTAR M060
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