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ADEOS 2

NORAD 27597 Payload LEO 2002-056A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
792 km
Apogee
795 km
Inclination
98.8°
Period
100.8 min
Mean Motion
14.29350769 rev/day
TLE Epoch
2026-06-19 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude794 km
Orbital Velocity26,852 km/h
Velocity7.46 km/s
Orbital Period101 minutes
Orbits / Day14.29
Eccentricity0.0002
Semi-Major Axis7,165 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
2002-12-14
Launch Site
TNSTA
Int'l Designator
2002-056A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ADEOS 2 is an active satellite operated by Japan, launched on 2002-12-14 from TNSTA. With over 24 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 792 km and 795 km with an inclination of 98.8°. It travels at approximately 26,852 km/h (7.46 km/s), completing one full orbit every 101 minutes — that’s roughly 14.29 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. Orbital Radar tracks ADEOS 2 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
ADEOS 2 orbits at an average altitude of 794 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of ADEOS 2’s average altitude, there are currently 429 active payloads and 2,274 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 98.8°, ADEOS 2 passes over latitudes between 98.8°N and 98.8°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. Japan operates approximately 189 active satellites in total, of which 9 share a similar altitude band with ADEOS 2.
❓ Frequently Asked Questions
ADEOS 2 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 794 km altitude. Its 98.8° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 101 minutes, travelling at 26,852 km/h.
ADEOS 2 is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 27597. You can track ADEOS 2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ADEOS 2 was launched on 2002-12-14 from TNSTA. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks ADEOS 2 (NORAD ID 27597) 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.
ADEOS 2 travels at approximately 26,852 km/h (16,685 mph) — roughly 7.46 km/s. It completes 14.29 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.