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ALOS

NORAD 28931 Payload LEO 2006-002A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
660 km
Apogee
662 km
Inclination
98.1°
Period
98.0 min
Mean Motion
14.70053646 rev/day
TLE Epoch
2026-06-19 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude661 km
Orbital Velocity27,104 km/h
Velocity7.53 km/s
Orbital Period98 minutes
Orbits / Day14.70
Eccentricity0.0001
Semi-Major Axis7,032 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
2006-01-24
Launch Site
TNSTA
Int'l Designator
2006-002A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ALOS is an active satellite operated by Japan, launched on 2006-01-24 from TNSTA. With over 20 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 660 km and 662 km with an inclination of 98.1°. It travels at approximately 27,104 km/h (7.53 km/s), completing one full orbit every 98 minutes — that’s roughly 14.70 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 ~10–25 years. Orbital Radar tracks ALOS in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
ALOS orbits at an average altitude of 661 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 ALOS’s average altitude, there are currently 658 active payloads and 1,117 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, LANDSAT 9. With an inclination of 98.1°, ALOS passes over latitudes between 98.1°N and 98.1°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 20 share a similar altitude band with ALOS.
❓ Frequently Asked Questions
ALOS is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 661 km altitude. Its 98.1° 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 98 minutes, travelling at 27,104 km/h.
ALOS is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 28931. You can track ALOS in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ALOS was launched on 2006-01-24 from TNSTA. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks ALOS (NORAD ID 28931) 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.
ALOS travels at approximately 27,104 km/h (16,842 mph) — roughly 7.53 km/s. It completes 14.70 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.