EKRAN 13
NORAD 15219
Payload
GEO
1984-090A
● Active
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GEO · NORAD 15219
NOW PASSING OVER
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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
36955 km
Apogee
37087 km
Inclination
10.9°
Period
1499.6 min
Mean Motion
0.96025734 rev/day
TLE Epoch
2026-05-08 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude37,021 km
Orbital Velocity10,911 km/h
Velocity3.03 km/s
Orbital Period25.0 hours
Orbits / Day0.96
Eccentricity0.0015
Semi-Major Axis43,392 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1984-08-24
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1984-090A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
EKRAN 13 is an active satellite operated by Russia (CIS), launched on 1984-08-24 from Baikonur, Kazakhstan. With over 42 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,955 km and 37,087 km with an inclination of 10.9°. It travels at approximately 10,911 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 EKRAN 13 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 13 occupies geostationary orbit (GEO) at approximately 35,786 km above the equator. At this precise altitude, the satellite’s orbital period matches the Earth’s rotation — so it appears to hover over a fixed point on the equator. GEO is used primarily for broadcast television, weather monitoring (Meteosat, GOES) and wideband communications. Only about 560 active satellites occupy the GEO belt, but its commercial value is immense: a single GEO slot can cover roughly one-third of the Earth’s surface. This satellite has a non-zero inclination of 10.9°, meaning it traces a small figure-of-eight pattern relative to the ground rather than remaining perfectly stationary. This can indicate an aging satellite whose stationkeeping fuel is running low, or a deliberate inclined-orbit strategy to extend operational life.
❓ Frequently Asked Questions
EKRAN 13 orbits at approximately 37,021 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 10,911 km/h — it just keeps pace with the ground below. With an inclination of 10.9°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed.
EKRAN 13 is operated by Russia (CIS). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 15219. You can track EKRAN 13 in real time on Orbital Radar’s live tracker.
EKRAN 13 was launched on 1984-08-24 from Baikonur, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan.
Yes — Orbital Radar tracks EKRAN 13 (NORAD ID 15219) 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.
EKRAN 13 travels at approximately 10,911 km/h (6,780 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.