TURKMENALEM52E/MONACOSAT

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TURKMENALEM52E/MONACOSAT is classified as:

Geostationary

NORAD ID: 40617

Int'l Code: 2015-023A

Perigee: 35,782.9 km

Apogee: 35,805.3 km

Inclination: 0.0 °

Period: 1,436.1 minutes

Semi major axis: 42165 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.

1 40617U 15023A   25196.49758356  .00000111  00000-0  00000-0 0  9992
2 40617   0.0273  95.0451 0002656  18.3665  51.3168  1.00270593 37476

Source of the keplerian elements: AFSPC