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NATO 4A

NORAD 21047 Payload GEO 1991-001A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
36337 km
Apogee
36369 km
Inclination
13.0°
Period
1465.1 min
Mean Motion
0.98284986 rev/day
TLE Epoch
2026-05-08 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,353 km
Orbital Velocity10,996 km/h
Velocity3.05 km/s
Orbital Period24.4 hours
Orbits / Day0.98
Eccentricity0.0004
Semi-Major Axis42,724 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
NATO
Launch Date
1991-01-08
Launch Site
Cape Canaveral, Florida
Int'l Designator
1991-001A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
NATO 4A is an active satellite operated by NATO, launched on 1991-01-08 from Cape Canaveral, Florida. With over 35 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,337 km and 36,369 km with an inclination of 13.0°. It travels at approximately 10,996 km/h (3.05 km/s), completing one full orbit every 24.4 hours — that’s roughly 0.98 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 NATO 4A in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
NATO 4A 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 13.0°, 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
NATO 4A orbits at approximately 36,353 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 10,996 km/h — it just keeps pace with the ground below. With an inclination of 13.0°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed.
NATO 4A is operated by NATO. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 21047. You can track NATO 4A in real time on Orbital Radar’s live tracker.
NATO 4A was launched on 1991-01-08 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.
Yes — Orbital Radar tracks NATO 4A (NORAD ID 21047) 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.
NATO 4A travels at approximately 10,996 km/h (6,833 mph) — roughly 3.05 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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