NORAD 40617
TURKMENALEM 52E/MONACOSA
Time
- Local time
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Position
- Latitude
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- Longitude
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- Altitude
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Speed
- Miles per hour
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- Kilometers per second
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- Miles per second
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From your location
- Azimuth
- -
- Elevation
- -
- Right ascension
- -
- Declination
- -
- Local sidereal time
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Sunlight
- Day / night
- -
Identity
- NORAD ID
- 40617
- International designator
- 2015-023A
- Launch date
- Apr 27, 2015
- Launch site
- AIR FORCE EASTERN TEST RANGE
- Radar size (RCS)
- Large (over 1 m²)
Radio
- Uplink
- -
- Downlink
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- Beacon
- -
- Mode
- -
Active transmitters from SatNOGS DB, licensed CC BY-SA 4.0.
Your station
- Grid locator
- -
Live
- Azimuth
- -
- Elevation
- -
- Range
- -
- Range rate
- -
- Naked-eye visibility
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- Sub-satellite grid
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- Footprint diameter
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Upcoming passes
Next 48 h · your local timeUse your location to predict passes.
Mutual visibility
With another station · next 48 hUse your location to find mutual windows.
Transmitters
Nominal · add location for Doppler-
Recent receptions
SatNOGS Network-
Orbit data
- TLE epoch
- 2026-11-02 11:31:35 UTC
- TLE age
- -
Radio data from SatNOGS DB and SatNOGS Network, licensed CC BY-SA 4.0.
Its orbit in 3D
Goes round Earth once every 23.9 hours, on an orbit tilted 0.0° from the equator, between 35,796 and 35,804 km up. Earth is drawn to scale.
Drag to turn · pinch to zoom · it moves live
About TURKMENALEM 52E/MONACOSA
TURKMENALEM 52E/MONACOSA is a satellite from TMMC, launched on Apr 27, 2015 from Air Force Eastern Test Range.
It sits in geostationary orbit about 35,800 km above the equator near 52°E, turning with Earth so it stays over the same spot.
The map shows where it is right now; the pass list tells you when it next comes over your location.
TürkmenÄlem 52°E · Turkmenistani communications satellite
- Operated by
- MonacoSAT, Turkmenistan National Space Agency
- Built by
- Thales Alenia Space
- Mass
- 4,707 kg
Wikipedia article ↗ · Names and facts: Wikidata (CC0).
Orbit height over the past year
Over the last 22 days its lowest point went from 35,774 km to 35,774 km. Sudden rises are engine burns that lift the orbit; slow declines are drag from the thin upper atmosphere.
From Space-Track element sets, one point a day.