SKYNET 5C
NORAD 33055
Payload
GEO
2008-030A
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GEO · NORAD 33055
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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
35770 km
Apogee
35804 km
Inclination
3.8°
Period
1436.1 min
Mean Motion
1.00271670 rev/day
TLE Epoch
2026-06-19 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,787 km
Orbital Velocity11,070 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0004
Semi-Major Axis42,158 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇬🇧 Ministry of Defense/Paradigm Secure Communications (wholly owned by EADS Astrium) (United Kingdom)
Launch Date
2008-06-12
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
2008-030A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
SKYNET 5C is an active satellite operated by Ministry of Defense/Paradigm Secure Communications (wholly owned by EADS Astrium) (United Kingdom), launched on 2008-06-12 from Guiana Space Centre, Kourou. After 18 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Geostationary Orbit (GEO) at altitudes between 35,770 km and 35,804 km with an inclination of 3.8°. 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 5C 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 5C 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 3.8°, 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 5C’s average altitude, there are currently 713 active payloads and 59 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 5C.
❓ Frequently Asked Questions
SKYNET 5C orbits at approximately 35,787 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 3.8°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
SKYNET 5C is operated by Ministry of Defense/Paradigm Secure Communications (wholly owned by EADS Astrium) (United Kingdom). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 33055. You can track SKYNET 5C in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SKYNET 5C was launched on 2008-06-12 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 5C (NORAD ID 33055) 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 5C 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.