EKRAN 21
NORAD 26736
Payload
GEO
2001-014A
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GEO · NORAD 26736
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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
35856 km
Apogee
36105 km
Inclination
14.6°
Period
1446.0 min
Mean Motion
0.99583930 rev/day
TLE Epoch
2026-06-19 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,981 km
Orbital Velocity11,044 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0029
Semi-Major Axis42,352 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2001-04-07
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2001-014A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
EKRAN 21 is an active satellite operated by Russia (CIS), launched on 2001-04-07 from Baikonur, Kazakhstan. With over 25 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,856 km and 36,105 km with an inclination of 14.6°. It travels at approximately 11,044 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 21 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 21 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 14.6°, 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 21’s average altitude, there are currently 50 active payloads and 27 tracked debris or rocket body fragments. Russia (CIS) operates approximately 1,286 active satellites in total, of which 2 share a similar altitude band with EKRAN 21.
❓ Frequently Asked Questions
EKRAN 21 orbits at approximately 35,981 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 11,044 km/h — it just keeps pace with the ground below. With an inclination of 14.6°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
EKRAN 21 is operated by Russia (CIS). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 26736. You can track EKRAN 21 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
EKRAN 21 was launched on 2001-04-07 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 EKRAN 21 (NORAD ID 26736) 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 21 travels at approximately 11,044 km/h (6,863 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.