SKYNET 4E
NORAD 25639
Payload
GEO
1999-009B
● Active
CONNECTING…
GEO · NORAD 25639
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
36134 km
Apogee
36144 km
Inclination
12.1°
Period
1454.1 min
Mean Motion
0.99029033 rev/day
TLE Epoch
2026-06-19 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,139 km
Orbital Velocity11,024 km/h
Velocity3.06 km/s
Orbital Period24.2 hours
Orbits / Day0.99
Eccentricity0.0001
Semi-Major Axis42,510 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇬🇧 Ministry of Defense (United Kingdom)
Launch Date
1999-02-26
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1999-009B
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
SKYNET 4E is an active satellite operated by Ministry of Defense (United Kingdom), launched on 1999-02-26 from Guiana Space Centre, Kourou. With over 27 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,134 km and 36,144 km with an inclination of 12.1°. It travels at approximately 11,024 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 4E 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 4E 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 12.1°, 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 SKYNET 4E’s average altitude, there are currently 185 active payloads and 8 tracked debris or rocket body fragments. United Kingdom operates approximately 720 active satellites in total, of which 3 share a similar altitude band with SKYNET 4E.
❓ Frequently Asked Questions
SKYNET 4E orbits at approximately 36,139 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 11,024 km/h — it just keeps pace with the ground below. With an inclination of 12.1°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
SKYNET 4E is operated by Ministry of Defense (United Kingdom). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 25639. You can track SKYNET 4E in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SKYNET 4E was launched on 1999-02-26 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 SKYNET 4E (NORAD ID 25639) 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.
SKYNET 4E travels at approximately 11,024 km/h (6,850 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.