THOR 1 (MARCOPOLO 2)
NORAD 20762
Payload
GEO
1990-074A
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GEO · NORAD 20762
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🛰️ Orbital Parameters
Perigee
36076 km
Apogee
36097 km
Inclination
14.6°
Period
1451.5 min
Mean Motion
0.99211290 rev/day
TLE Epoch
2026-06-18 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,087 km
Orbital Velocity11,030 km/h
Velocity3.06 km/s
Orbital Period24.2 hours
Orbits / Day0.99
Eccentricity0.0002
Semi-Major Axis42,458 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇳🇴 Norway
Launch Date
1990-08-18
Launch Site
Cape Canaveral, Florida
Int'l Designator
1990-074A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
THOR 1 (MARCOPOLO 2) is an active satellite operated by Norway, launched on 1990-08-18 from Cape Canaveral, Florida. With over 36 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,076 km and 36,097 km with an inclination of 14.6°. It travels at approximately 11,030 km/h (3.06 km/s), completing one full orbit every 24.2 hours — that’s roughly 0.99 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 THOR 1 (MARCOPOLO 2) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
THOR 1 (MARCOPOLO 2) 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 THOR 1 (MARCOPOLO 2)’s average altitude, there are currently 150 active payloads and 11 tracked debris or rocket body fragments. Norway operates approximately 26 active satellites in total.
❓ Frequently Asked Questions
THOR 1 (MARCOPOLO 2) orbits at approximately 36,087 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 11,030 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.
THOR 1 (MARCOPOLO 2) is operated by Norway. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 20762. You can track THOR 1 (MARCOPOLO 2) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
THOR 1 (MARCOPOLO 2) was launched on 1990-08-18 from Cape Canaveral, Florida, one of the busiest launch facilities in the world, operated by NASA and the U.S. Space Force on Florida’s Atlantic coast. View the full satellite launch log.
Yes — Orbital Radar tracks THOR 1 (MARCOPOLO 2) (NORAD ID 20762) 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.
THOR 1 (MARCOPOLO 2) travels at approximately 11,030 km/h (6,854 mph) — roughly 3.06 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.