RADUGA 20
NORAD 17611
Payload
GEO
1987-028A
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GEO · NORAD 17611
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
36924 km
Apogee
37155 km
Inclination
13.3°
Period
1500.6 min
Mean Motion
0.95962045 rev/day
TLE Epoch
2026-06-19 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude37,040 km
Orbital Velocity10,909 km/h
Velocity3.03 km/s
Orbital Period25.0 hours
Orbits / Day0.96
Eccentricity0.0027
Semi-Major Axis43,411 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1987-03-19
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1987-028A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
RADUGA 20 is an active satellite operated by Russia (CIS), launched on 1987-03-19 from Baikonur, Kazakhstan. With over 39 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,924 km and 37,155 km with an inclination of 13.3°. It travels at approximately 10,909 km/h (3.03 km/s), completing one full orbit every 25.0 hours — that’s roughly 0.96 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 RADUGA 20 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
RADUGA 20 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. With an inclination of 13.3°, it traces a small figure-of-eight pattern relative to the equator rather than remaining perfectly stationary, which can indicate aging stationkeeping fuel or a deliberate inclined-orbit strategy. Within ±50 km of RADUGA 20’s average altitude, there are currently 7 active payloads and 3 tracked debris or rocket body fragments. Russia (CIS) operates approximately 1,286 active satellites in total, of which 4 share a similar altitude band with RADUGA 20.
❓ Frequently Asked Questions
RADUGA 20 orbits at approximately 37,040 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 10,909 km/h — it just keeps pace with the ground below. With an inclination of 13.3°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
RADUGA 20 is operated by Russia (CIS). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 17611. You can track RADUGA 20 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
RADUGA 20 was launched on 1987-03-19 from Baikonur, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. View the full satellite launch log.
Yes — Orbital Radar tracks RADUGA 20 (NORAD ID 17611) 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.
RADUGA 20 travels at approximately 10,909 km/h (6,778 mph) — roughly 3.03 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.