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OLYMPUS 1

NORAD 20122 Payload GEO 1989-053A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
35428 km
Apogee
35537 km
Inclination
12.2°
Period
1420.6 min
Mean Motion
1.01367739 rev/day
TLE Epoch
2026-06-19 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,483 km
Orbital Velocity11,110 km/h
Velocity3.09 km/s
Orbital Period23 hours 41 minutes
Orbits / Day1.01
Eccentricity0.0013
Semi-Major Axis41,854 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
ESA (European Space Agency)
Launch Date
1989-07-12
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1989-053A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
OLYMPUS 1 is an active satellite operated by ESA (European Space Agency), launched on 1989-07-12 from Guiana Space Centre, Kourou. With over 37 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,428 km and 35,537 km with an inclination of 12.2°. It travels at approximately 11,110 km/h (3.09 km/s), completing one full orbit every 23 hours 41 minutes — that’s roughly 1.01 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 OLYMPUS 1 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
OLYMPUS 1 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 12.2°, 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 OLYMPUS 1’s average altitude, there are currently 3 active payloads and 28 tracked debris or rocket body fragments. ESA (European Space Agency) operates approximately 93 active satellites in total.
❓ Frequently Asked Questions
OLYMPUS 1 orbits at approximately 35,483 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 11,110 km/h — it just keeps pace with the ground below. With an inclination of 12.2°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
OLYMPUS 1 is operated by ESA (European Space Agency). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 20122. You can track OLYMPUS 1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
OLYMPUS 1 was launched on 1989-07-12 from Guiana Space Centre, Kourou, the European spaceport in French Guiana, chosen for its equatorial location which provides an energy-efficient boost for orbital insertions. View the full satellite launch log.
Yes — Orbital Radar tracks OLYMPUS 1 (NORAD ID 20122) 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.
OLYMPUS 1 travels at approximately 11,110 km/h (6,903 mph) — roughly 3.09 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.