ALOS-4
NORAD 60182
Payload
LEO
2024-123A
● Active
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LEO · NORAD 60182
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
630 km
Apogee
632 km
Inclination
97.9°
Period
97.3 min
Mean Motion
14.79471668 rev/day
TLE Epoch
2026-06-19 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude631 km
Orbital Velocity27,162 km/h
Velocity7.54 km/s
Orbital Period97 minutes
Orbits / Day14.79
Eccentricity0.0001
Semi-Major Axis7,002 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
2024-07-01
Launch Site
TNSTA
Int'l Designator
2024-123A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ALOS-4 is an active satellite operated by Japan, launched on 2024-07-01 from TNSTA. It orbits in Low Earth Orbit (LEO) at altitudes between 630 km and 632 km with an inclination of 97.9°. It travels at approximately 27,162 km/h (7.54 km/s), completing one full orbit every 97 minutes — that’s roughly 14.79 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-4 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-4 orbits at an average altitude of 631 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-4’s average altitude, there are currently 790 active payloads and 843 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050. With an inclination of 97.9°, ALOS-4 passes over latitudes between 97.9°N and 97.9°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 23 share a similar altitude band with ALOS-4.
❓ Frequently Asked Questions
ALOS-4 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 631 km altitude. Its 97.9° 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 97 minutes, travelling at 27,162 km/h.
ALOS-4 is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 60182. You can track ALOS-4 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ALOS-4 was launched on 2024-07-01 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-4 (NORAD ID 60182) 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-4 travels at approximately 27,162 km/h (16,878 mph) — roughly 7.54 km/s. It completes 14.79 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.