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EKRAN 7

NORAD 12564 Payload GEO 1981-061A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
35788 km
Apogee
35818 km
Inclination
6.3°
Period
1436.9 min
Mean Motion
1.00214368 rev/day
TLE Epoch
2026-09-17 15:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,803 km
Orbital Velocity11,067 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0004
Semi-Major Axis42,174 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 MSvyaz (Russia (CIS))
Launch Date
1981-06-26
Launch Site
Baikonur Cosmodrome, Kazakhstan
Int'l Designator
1981-061A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
EKRAN 7 is an active satellite operated by MSvyaz (Russia (CIS)), launched on 1981-06-26 from Baikonur Cosmodrome, Kazakhstan on the Ekran No. 21L launch. With over 45 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,788 km and 35,818 km with an inclination of 6.3°. 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 EKRAN 7 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
EKRAN 7 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 6.3°, 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 EKRAN 7’s average altitude, there are currently 741 active payloads and 56 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. Russia (CIS) operates approximately 1,536 active satellites in total, of which 127 share a similar altitude band with EKRAN 7.
❓ Frequently Asked Questions
EKRAN 7 orbits at approximately 35,803 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 6.3°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
EKRAN 7 is operated by MSvyaz (Russia (CIS)). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 12564. You can track EKRAN 7 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
EKRAN 7 was launched on 1981-06-26 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 EKRAN 7 (NORAD ID 12564) 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.
EKRAN 7 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.