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TURKMENALEM52E/MONACOSAT

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TURKMENALEM52E/MONACOSAT is classified as:


NORAD ID: 40617
Int'l Code: 2015-023A
Perigee: 35,786.2 km
Apogee: 35,800.5 km
Inclination: 0.0 °
Period: 1,436.1 minutes
Semi major axis: 42164 km
RCS: Unknown
Launch date: April 27, 2015
Source: TURKMENISTAN/MONACO (TMMC)
Launch site: AIR FORCE EASTERN TEST RANGE (AFETR)

TURKMENALEM52E/MONACOSAT is a communications satellite, the 1st satellite of Turkmenistan, designed for a lifetime of at least 16 years. Destination of this geostationary satellite is 52 degrees east longitude. The 52 degrees east slot is registered to Monaco by the International Telecommunications Union. The operating location and Monaco's role in the mission help give the TurkmenAlem52E/MonacoSat satellite its unusual name. The satellite will reach users across Central Asia, Europe and Africa, with a coverage zone spanning more than 90 countries.
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NASA's NSSDC Master Catalog

Two Line Element Set (TLE):
1 40617U 15023A   17350.61814441 +.00000108 +00000-0 +00000-0 0  9993
2 40617 000.0203 050.5642 0001688 229.5498 079.8746 01.00273213009716
Source of the keplerian elements: AFSPC