SKYNET 4C
NORAD 20776
Payload
GEO
1990-079A
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GEO · NORAD 20776
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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
35776 km
Apogee
35796 km
Inclination
13.3°
Period
1436.1 min
Mean Motion
1.00274127 rev/day
TLE Epoch
2026-06-11 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,786 km
Orbital Velocity11,070 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0002
Semi-Major Axis42,157 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇬🇧 Intelsat/Paradigm Secure Communications (wholly owned by EADS Astrium) (United Kingdom)
Launch Date
1990-08-30
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1990-079A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
SKYNET 4C is an active satellite operated by Intelsat/Paradigm Secure Communications (wholly owned by EADS Astrium) (United Kingdom), launched on 1990-08-30 from Guiana Space Centre, Kourou. With over 36 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,776 km and 35,796 km with an inclination of 13.3°. It travels at approximately 11,070 km/h (3.07 km/s), completing one full orbit every ~24 hours (geosynchronous) — that’s roughly 1.00 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 4C 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 4C 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 13.3°, 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 4C’s average altitude, there are currently 713 active payloads and 58 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. United Kingdom operates approximately 720 active satellites in total, of which 13 share a similar altitude band with SKYNET 4C.
❓ Frequently Asked Questions
SKYNET 4C orbits at approximately 35,786 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 11,070 km/h — it just keeps pace with the ground below. With an inclination of 13.3°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
SKYNET 4C is operated by Intelsat/Paradigm Secure Communications (wholly owned by EADS Astrium) (United Kingdom). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 20776. You can track SKYNET 4C in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SKYNET 4C was launched on 1990-08-30 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 4C (NORAD ID 20776) 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 4C travels at approximately 11,070 km/h (6,878 mph) — roughly 3.07 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.