TURKMENALEM 52E/MONACOSA
NORAD 40617
Payload
GEO
2015-023A
● Active
CONNECTING…
GEO · NORAD 40617
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
35775 km
Apogee
35798 km
Inclination
0.0°
Period
1436.1 min
Mean Motion
1.00271926 rev/day
TLE Epoch
2026-06-19 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,787 km
Orbital Velocity11,070 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0003
Semi-Major Axis42,158 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
Turkmenistan Ministry of Communications/SSI-Monaco (TMMC)
Launch Date
2015-04-27
Launch Site
Cape Canaveral, Florida
Int'l Designator
2015-023A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
TURKMENALEM 52E/MONACOSA is an active satellite operated by Turkmenistan Ministry of Communications/SSI-Monaco (TMMC), launched on 2015-04-27 from Cape Canaveral, Florida. After 11 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Geostationary Orbit (GEO) at altitudes between 35,775 km and 35,798 km with an inclination of 0.0°. It travels at approximately 11,070 km/h (3.07 km/s), completing one full orbit every ~24 hours (geosynchronous) — that’s roughly 1.00 orbits per day. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Orbital Radar tracks TURKMENALEM 52E/MONACOSA in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
TURKMENALEM 52E/MONACOSA occupies geostationary orbit at approximately 35,786 km above the equator, where its orbital period matches the Earth’s 24-hour rotation. From the ground, it appears to hover over a fixed point — ideal for broadcast television, weather monitoring and wideband communications. Within ±50 km of TURKMENALEM 52E/MONACOSA’s average altitude, there are currently 713 active payloads and 58 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13.
❓ Frequently Asked Questions
TURKMENALEM 52E/MONACOSA orbits at approximately 35,787 km altitude, where the orbital period matches the Earth’s 24-hour rotation. This means it stays above the same point on the equator at all times. Its actual speed is still 11,070 km/h — it just keeps pace with the ground below. Learn more about geostationary orbits.
TURKMENALEM 52E/MONACOSA is operated by Turkmenistan Ministry of Communications/SSI-Monaco (TMMC). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 40617. You can track TURKMENALEM 52E/MONACOSA in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
TURKMENALEM 52E/MONACOSA was launched on 2015-04-27 from Cape Canaveral, Florida, one of the busiest launch facilities in the world, operated by NASA and the U.S. Space Force on Florida’s Atlantic coast. View the full satellite launch log.
Yes — Orbital Radar tracks TURKMENALEM 52E/MONACOSA (NORAD ID 40617) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
TURKMENALEM 52E/MONACOSA travels at approximately 11,070 km/h (6,878 mph) — roughly 3.07 km/s. Despite this high speed, it appears stationary from the ground because it matches the Earth’s rotation. Geostationary satellites are actually slower than LEO satellites because orbital velocity decreases with altitude.