EKRAN 19
NORAD 19683
Payload
GEO
1988-108A
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GEO · NORAD 19683
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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
36717 km
Apogee
36948 km
Inclination
13.6°
Period
1489.9 min
Mean Motion
0.96653218 rev/day
TLE Epoch
2026-06-19 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,833 km
Orbital Velocity10,935 km/h
Velocity3.04 km/s
Orbital Period24.8 hours
Orbits / Day0.97
Eccentricity0.0027
Semi-Major Axis43,204 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1988-12-10
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1988-108A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
EKRAN 19 is an active satellite operated by Russia (CIS), launched on 1988-12-10 from Baikonur, Kazakhstan. With over 38 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,717 km and 36,948 km with an inclination of 13.6°. It travels at approximately 10,935 km/h (3.04 km/s), completing one full orbit every 24.8 hours — that’s roughly 0.97 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 19 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 19 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 13.6°, 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 19’s average altitude, there are currently 7 active payloads and 2 tracked debris or rocket body fragments. Russia (CIS) operates approximately 1,285 active satellites in total, of which 4 share a similar altitude band with EKRAN 19.
❓ Frequently Asked Questions
EKRAN 19 orbits at approximately 36,833 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 10,935 km/h — it just keeps pace with the ground below. With an inclination of 13.6°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
EKRAN 19 is operated by Russia (CIS). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 19683. You can track EKRAN 19 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
EKRAN 19 was launched on 1988-12-10 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 19 (NORAD ID 19683) 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 19 travels at approximately 10,935 km/h (6,795 mph) — roughly 3.04 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.