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RADUGA 23

NORAD 19928 Payload GEO 1989-030A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
35723 km
Apogee
35887 km
Inclination
11.8°
Period
1437.0 min
Mean Motion
1.00206470 rev/day
TLE Epoch
2026-06-18 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,805 km
Orbital Velocity11,067 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0019
Semi-Major Axis42,176 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1989-04-14
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1989-030A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
RADUGA 23 is an active satellite operated by Russia (CIS), launched on 1989-04-14 from Baikonur, Kazakhstan. With over 37 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,723 km and 35,887 km with an inclination of 11.8°. It travels at approximately 11,067 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 RADUGA 23 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 23 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 11.8°, 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 23’s average altitude, there are currently 713 active payloads and 64 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. Russia (CIS) operates approximately 1,285 active satellites in total, of which 122 share a similar altitude band with RADUGA 23.
❓ Frequently Asked Questions
RADUGA 23 orbits at approximately 35,805 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 11,067 km/h — it just keeps pace with the ground below. With an inclination of 11.8°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
RADUGA 23 is operated by Russia (CIS). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 19928. You can track RADUGA 23 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
RADUGA 23 was launched on 1989-04-14 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 23 (NORAD ID 19928) 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 23 travels at approximately 11,067 km/h (6,877 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.