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GEOTAIL

NORAD 22049 Payload MEO 1992-044A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
46986 km
Apogee
193939 km
Inclination
45.3°
Period
7492.8 min
Mean Motion
0.19218384 rev/day
TLE Epoch
2026-06-17 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude120,463 km
Orbital Velocity6,382 km/h
Velocity1.77 km/s
Orbital Period124.9 hours
Orbits / Day0.19
Eccentricity0.5793
Semi-Major Axis126,834 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇯🇵 Institute of Space and Astronautical Science (ISAS)/NASA/ESA (Japan)
Launch Date
1992-07-24
Launch Site
Cape Canaveral, Florida
Int'l Designator
1992-044A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
GEOTAIL is an active satellite operated by Institute of Space and Astronautical Science (ISAS)/NASA/ESA (Japan), launched on 1992-07-24 from Cape Canaveral, Florida. With over 34 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 46,986 km and 193,939 km with an inclination of 45.3°. It travels at approximately 6,382 km/h (1.77 km/s), completing one full orbit every 124.9 hours — that’s roughly 0.19 orbits per day. Its orbital eccentricity of 0.5793 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Orbital Radar tracks GEOTAIL in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
GEOTAIL orbits at an average altitude of 120,463 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. With an inclination of 45.3°, GEOTAIL passes over latitudes between 45.3°N and 45.3°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. Japan operates approximately 189 active satellites in total.
❓ Frequently Asked Questions
GEOTAIL orbits in Medium Earth Orbit (MEO) at altitudes between 46,986 km (perigee) and 193,939 km (apogee), with an average altitude of approximately 120,463 km. It completes one orbit every 124.9 hours, travelling at approximately 6,382 km/h (3,966 mph).
GEOTAIL is operated by Institute of Space and Astronautical Science (ISAS)/NASA/ESA (Japan). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 22049. You can track GEOTAIL in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
GEOTAIL was launched on 1992-07-24 from Cape Canaveral, Florida, one of the busiest launch facilities in the world, operated by NASA and the U.S. Space Force on Florida’s Atlantic coast. View the full satellite launch log.
Yes — Orbital Radar tracks GEOTAIL (NORAD ID 22049) 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.
GEOTAIL travels at approximately 6,382 km/h (3,966 mph) — roughly 1.77 km/s. It completes 0.19 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 0 sunrises and sunsets every 24 hours.