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TEAMSAT

NORAD 25025 Payload MEO 1997-066C ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
549 km
Apogee
26601 km
Inclination
7.9°
Period
467.5 min
Mean Motion
3.08027101 rev/day
TLE Epoch
2026-06-19 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude13,575 km
Orbital Velocity16,093 km/h
Velocity4.47 km/s
Orbital Period7 hours 47 minutes
Orbits / Day3.08
Eccentricity0.6531
Semi-Major Axis19,946 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
ESA (European Space Agency)
Launch Date
1997-10-30
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1997-066C
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
TEAMSAT is an active satellite operated by ESA (European Space Agency), launched on 1997-10-30 from Guiana Space Centre, Kourou. With over 29 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 549 km and 26,601 km with an inclination of 7.9°. It travels at approximately 16,093 km/h (4.47 km/s), completing one full orbit every 7 hours 47 minutes — that’s roughly 3.08 orbits per day. Its orbital eccentricity of 0.6531 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks TEAMSAT in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
TEAMSAT orbits at an average altitude of 13,575 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of TEAMSAT’s average altitude, there are currently 2 active payloads and 7 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 7.9°, TEAMSAT passes over latitudes between 7.9°N and 7.9°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. ESA (European Space Agency) operates approximately 93 active satellites in total, of which 2 share a similar altitude band with TEAMSAT.
❓ Frequently Asked Questions
TEAMSAT orbits in Medium Earth Orbit (MEO) at altitudes between 549 km (perigee) and 26,601 km (apogee), with an average altitude of approximately 13,575 km. It completes one orbit every 7 hours 47 minutes, travelling at approximately 16,093 km/h (10,000 mph).
TEAMSAT is operated by ESA (European Space Agency). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 25025. You can track TEAMSAT in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
TEAMSAT was launched on 1997-10-30 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. At its current altitude, the estimated remaining orbital lifetime is: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks TEAMSAT (NORAD ID 25025) 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.
TEAMSAT travels at approximately 16,093 km/h (10,000 mph) — roughly 4.47 km/s. It completes 3.08 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 6 sunrises and sunsets every 24 hours.