TURKMENALEM52E/MONACOSAT

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TURKMENALEM52E/MONACOSAT is classified as:

Geostationary

NORAD ID: 40617

Int'l Code: 2015-023A

Perigee: 35,779.3 km

Apogee: 35,808.2 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.

1 40617U 15023A   24325.78058240  .00000105  00000-0  00000-0 0  9995
2 40617   0.0332  81.8699 0003424 166.8709 144.5673  1.00271644 35091

Source of the keplerian elements: AFSPC