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AJISAI (EGS)

NORAD 16908 Payload LEO 1986-061A ● Active
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Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
1479 km
Apogee
1496 km
Inclination
50.0°
Period
115.7 min
Mean Motion
12.44515703 rev/day
TLE Epoch
2026-03-17 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,488 km
Orbital Velocity25,639 km/h
Velocity7.12 km/s
Orbital Period116 minutes
Orbits / Day12.45
Eccentricity0.0011
Semi-Major Axis7,859 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
1986-08-12
Launch Site
TNSTA
Int'l Designator
1986-061A
Object Type
Payload
RCS Size
Large (>1 m²)
🔗 Constellation / Groups
visualgeodetic
📖 About This Object
AJISAI (EGS) is an active satellite operated by Japan, launched on 1986-08-12 from TNSTA. With over 40 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 1,479 km and 1,496 km with an inclination of 50.0°. It travels at approximately 25,639 km/h (7.12 km/s), completing one full orbit every 116 minutes — that’s roughly 12.45 orbits per day. It is part of the Geodetic constellation group. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. Orbital Radar tracks AJISAI (EGS) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
AJISAI (EGS) orbits in the upper reaches of Low Earth Orbit, above 1,000 km. At this altitude, atmospheric drag is negligible and objects can remain in orbit for thousands of years without active deorbiting. This region is used by satellite broadband constellations like OneWeb and by scientific missions that need stable, long-duration orbits away from the densest debris bands. The high inclination typical at this altitude provides near-global coverage.
❓ Frequently Asked Questions
AJISAI (EGS) orbits in Low Earth Orbit (LEO) at altitudes between 1,479 km (perigee) and 1,496 km (apogee), with an average altitude of approximately 1,488 km. It completes one orbit every 116 minutes, travelling at approximately 25,639 km/h (15,931 mph).
AJISAI (EGS) is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 16908. You can track AJISAI (EGS) in real time on Orbital Radar’s live tracker.
AJISAI (EGS) was launched on 1986-08-12 from TNSTA. At its current altitude, the estimated remaining orbital lifetime is: thousands of years.
Yes — Orbital Radar tracks AJISAI (EGS) (NORAD ID 16908) 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.
AJISAI (EGS) travels at approximately 25,639 km/h (15,931 mph) — roughly 7.12 km/s. It completes 12.45 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 25 sunrises and sunsets every 24 hours.
AJISAI (EGS) is a member of the Geodetic constellation. Satellites in this group work together to provide coordinated coverage, typically in similar orbital planes at comparable altitudes. You can view all Geodetic satellites on Orbital Radar’s live tracker.