RADUGA 2
NORAD 9416
Payload
GEO
1976-092A
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Altitude (km)
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Latitude
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🛰️ Orbital Parameters
Perigee
35658 km
Apogee
35900 km
Inclination
3.2°
Period
1435.7 min
Mean Motion
1.00298250 rev/day
TLE Epoch
2026-10-21 02:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,779 km
Orbital Velocity11,071 km/h
Velocity3.08 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0029
Semi-Major Axis42,150 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 GUKOS RVSN (Russia (CIS))
Launch Date
1976-09-11
Launch Site
Baikonur Cosmodrome, Kazakhstan
Int'l Designator
1976-092A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
RADUGA 2 is an active satellite operated by GUKOS RVSN (Russia (CIS)), launched on 1976-09-11 from Baikonur Cosmodrome, Kazakhstan on the Gran' No. 12L launch. After more than 50 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Geostationary Orbit (GEO) at altitudes between 35,658 km and 35,900 km with an inclination of 3.2°. It travels at approximately 11,071 km/h (3.08 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 2 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 2 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 3.2°, 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 2’s average altitude, there are currently 737 active payloads and 57 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. Russia (CIS) operates approximately 1,553 active satellites in total, of which 128 share a similar altitude band with RADUGA 2.
❓ Frequently Asked Questions
RADUGA 2 orbits at approximately 35,779 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 11,071 km/h — it just keeps pace with the ground below. With an inclination of 3.2°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
RADUGA 2 is operated by GUKOS RVSN (Russia (CIS)). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 9416. You can track RADUGA 2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
RADUGA 2 was launched on 1976-09-11 from Baikonur Cosmodrome, 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 2 (NORAD ID 9416) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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 2 travels at approximately 11,071 km/h (6,879 mph) — roughly 3.08 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.