SKYNET 4A
NORAD 20401
Payload
GEO
1990-001A
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GEO · NORAD 20401
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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
36086 km
Apogee
36209 km
Inclination
12.5°
Period
1454.6 min
Mean Motion
0.98998258 rev/day
TLE Epoch
2026-05-08 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,148 km
Orbital Velocity11,023 km/h
Velocity3.06 km/s
Orbital Period24.2 hours
Orbits / Day0.99
Eccentricity0.0014
Semi-Major Axis42,519 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇬🇧 United Kingdom
Launch Date
1990-01-01
Launch Site
Cape Canaveral, Florida
Int'l Designator
1990-001A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
SKYNET 4A is an active satellite operated by United Kingdom, launched on 1990-01-01 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 36,086 km and 36,209 km with an inclination of 12.5°. It travels at approximately 11,023 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 SKYNET 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
SKYNET 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 12.5°, 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
SKYNET 4A orbits at approximately 36,148 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 11,023 km/h — it just keeps pace with the ground below. With an inclination of 12.5°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed.
SKYNET 4A is operated by United Kingdom. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 20401. You can track SKYNET 4A in real time on Orbital Radar’s live tracker.
SKYNET 4A was launched on 1990-01-01 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 SKYNET 4A (NORAD ID 20401) 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.
SKYNET 4A travels at approximately 11,023 km/h (6,849 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.