MARECS B2
NORAD 15386
Payload
GEO
1984-114B
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GEO · NORAD 15386
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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
36559 km
Apogee
37541 km
Inclination
13.5°
Period
1501.1 min
Mean Motion
0.95928759 rev/day
TLE Epoch
2026-06-19 12:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude37,050 km
Orbital Velocity10,907 km/h
Velocity3.03 km/s
Orbital Period25.0 hours
Orbits / Day0.96
Eccentricity0.0113
Semi-Major Axis43,421 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
ESA (European Space Agency)
Launch Date
1984-11-10
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1984-114B
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
MARECS B2 is an active satellite operated by ESA (European Space Agency), launched on 1984-11-10 from Guiana Space Centre, Kourou. With over 42 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,559 km and 37,541 km with an inclination of 13.5°. It travels at approximately 10,907 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 MARECS B2 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 B2 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 13.5°, 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 MARECS B2’s average altitude, there are currently 7 active payloads and 2 tracked debris or rocket body fragments. ESA (European Space Agency) operates approximately 93 active satellites in total.
❓ Frequently Asked Questions
MARECS B2 orbits at approximately 37,050 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 10,907 km/h — it just keeps pace with the ground below. With an inclination of 13.5°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
MARECS B2 is operated by ESA (European Space Agency). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 15386. You can track MARECS B2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
MARECS B2 was launched on 1984-11-10 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 MARECS B2 (NORAD ID 15386) 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.
MARECS B2 travels at approximately 10,907 km/h (6,778 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.