GLOBALSTAR M040
1999-02-09
Satellite information GLOBALSTAR M040 - Globalstar M040
| Spacetrack Directory Name | GLOBALSTAR M040 |
| Alternative name | Globalstar M040 |
| Group | GLOBALSTAR |
| Orbit launches |
1999-02-09 |
| Deorbitation |
|
| Country/organisation of origin | Globalstar (GLOB) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Type | Satellite |
| Categories | |
| Perigee | 1415 km |
| Apogee | 1416 km |
Additional information GLOBALSTAR M040
GLOBALSTAR M040 is a communication satellite with the OBJECT_ID 1999-004B and NORAD_CAT_ID 25622. Manufactured by LOR, it was launched on February 9, 1999, from the TYMSC launch site using the Soyuz-U-PVB launch vehicle. The 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 configuration. It had a dry mass of 380 kilograms and a launch mass of 450 kilograms, powered by two deployable solar arrays and batteries. The mission of GLOBALSTAR M040 is communication, equipped with the LS-400 AOCS motor for attitude control. Its shape resembles a box with two panels, and it has an RCS of 1.891. The satellite was owned by GLOBT and carries the payload Globalstar FM40. It had a planned lifetime of 7.5 years from its launch date.
satellite GLOBALSTAR M040 Date of exalting 09.02.1999y.ISS
Buy us a coffee!
