THOR 2A
NORAD 24808
Payload
GEO
1997-025A
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🛰️ Orbital Parameters
Perigee
36139 km
Apogee
36173 km
Inclination
12.0°
Period
1455.0 min
Mean Motion
0.98969289 rev/day
TLE Epoch
2026-06-19 02:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,156 km
Orbital Velocity11,021 km/h
Velocity3.06 km/s
Orbital Period24.3 hours
Orbits / Day0.99
Eccentricity0.0004
Semi-Major Axis42,527 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇳🇴 Norway
Launch Date
1997-05-20
Launch Site
Cape Canaveral, Florida
Int'l Designator
1997-025A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
THOR 2A is an active satellite operated by Norway, launched on 1997-05-20 from Cape Canaveral, Florida. With over 29 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,139 km and 36,173 km with an inclination of 12.0°. It travels at approximately 11,021 km/h (3.06 km/s), completing one full orbit every 24.3 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 2A 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 2A 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 12.0°, 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 2A’s average altitude, there are currently 168 active payloads and 9 tracked debris or rocket body fragments. Norway operates approximately 26 active satellites in total, of which 2 share a similar altitude band with THOR 2A.
❓ Frequently Asked Questions
THOR 2A orbits at approximately 36,156 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 11,021 km/h — it just keeps pace with the ground below. With an inclination of 12.0°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
THOR 2A is operated by Norway. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 24808. You can track THOR 2A in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
THOR 2A was launched on 1997-05-20 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 2A (NORAD ID 24808) 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 2A travels at approximately 11,021 km/h (6,848 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.