S80/T
NORAD 22078
Payload
LEO
1992-052C
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LEO · NORAD 22078
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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
1301 km
Apogee
1327 km
Inclination
66.1°
Period
111.9 min
Mean Motion
12.86853408 rev/day
TLE Epoch
2026-06-19 14:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,314 km
Orbital Velocity25,927 km/h
Velocity7.20 km/s
Orbital Period112 minutes
Orbits / Day12.87
Eccentricity0.0017
Semi-Major Axis7,685 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇫🇷 France
Launch Date
1992-08-10
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1992-052C
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
S80/T is an active satellite operated by France, launched on 1992-08-10 from Guiana Space Centre, Kourou. With over 34 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 1,301 km and 1,327 km with an inclination of 66.1°. It travels at approximately 25,927 km/h (7.20 km/s), completing one full orbit every 112 minutes — that’s roughly 12.87 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. Orbital Radar tracks S80/T in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
S80/T orbits at an average altitude of 1,314 km in the uppermost reaches of Low Earth Orbit. At this altitude, orbital decay is effectively zero without active deorbiting, and coverage footprints are significantly larger than lower LEO, though at the cost of higher latency. Within ±50 km of S80/T’s average altitude, there are currently 13 active payloads and 261 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 66.1°, S80/T passes over latitudes between 66.1°N and 66.1°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. France operates approximately 115 active satellites in total, of which 2 share a similar altitude band with S80/T.
❓ Frequently Asked Questions
S80/T orbits in Low Earth Orbit (LEO) at altitudes between 1,301 km (perigee) and 1,327 km (apogee), with an average altitude of approximately 1,314 km. It completes one orbit every 112 minutes, travelling at approximately 25,927 km/h (16,110 mph).
S80/T is operated by France. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 22078. You can track S80/T in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
S80/T was launched on 1992-08-10 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. At its current altitude, the estimated remaining orbital lifetime is: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks S80/T (NORAD ID 22078) 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.
S80/T travels at approximately 25,927 km/h (16,110 mph) — roughly 7.20 km/s. It completes 12.87 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 26 sunrises and sunsets every 24 hours.