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MARECS A

NORAD 13010 Payload GEO 1981-122A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
36809 km
Apogee
37832 km
Inclination
11.7°
Period
1515.2 min
Mean Motion
0.95038986 rev/day
TLE Epoch
2026-05-08 15:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude37,321 km
Orbital Velocity10,874 km/h
Velocity3.02 km/s
Orbital Period25.3 hours
Orbits / Day0.95
Eccentricity0.0117
Semi-Major Axis43,692 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
ESA (European Space Agency)
Launch Date
1981-12-20
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1981-122A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
MARECS A is an active satellite operated by ESA (European Space Agency), launched on 1981-12-20 from Guiana Space Centre, Kourou. With over 45 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,809 km and 37,832 km with an inclination of 11.7°. It travels at approximately 10,874 km/h (3.02 km/s), completing one full orbit every 25.3 hours — that’s roughly 0.95 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 MARECS A in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
MARECS A 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 11.7°, 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
MARECS A orbits at approximately 37,321 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 10,874 km/h — it just keeps pace with the ground below. With an inclination of 11.7°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed.
MARECS A is operated by ESA (European Space Agency). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 13010. You can track MARECS A in real time on Orbital Radar’s live tracker.
MARECS A was launched on 1981-12-20 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.
Yes — Orbital Radar tracks MARECS A (NORAD ID 13010) 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.
MARECS A travels at approximately 10,874 km/h (6,757 mph) — roughly 3.02 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.
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