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HORYU 2

NORAD 38340 Payload LEO 2012-025D ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
589 km
Apogee
600 km
Inclination
98.2°
Period
96.6 min
Mean Motion
14.91080777 rev/day
TLE Epoch
2026-06-19 15:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude595 km
Orbital Velocity27,233 km/h
Velocity7.56 km/s
Orbital Period97 minutes
Orbits / Day14.91
Eccentricity0.0008
Semi-Major Axis6,966 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Kyushu Institute of Technology (KIT) (Japan)
Launch Date
2012-05-17
Launch Site
TNSTA
Int'l Designator
2012-025D
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
HORYU 2 is an active satellite operated by Kyushu Institute of Technology (KIT) (Japan), launched on 2012-05-17 from TNSTA. After 14 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 589 km and 600 km with an inclination of 98.2°. It travels at approximately 27,233 km/h (7.56 km/s), completing one full orbit every 97 minutes — that’s roughly 14.91 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 ~3–10 years. Orbital Radar tracks HORYU 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
HORYU 2 orbits at an average altitude of 595 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 HORYU 2’s average altitude, there are currently 2,119 active payloads and 626 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3005, STARLINK-3090. This makes it one of the more crowded altitude bands, containing roughly 12.2% of all active satellites. With an inclination of 98.2°, HORYU 2 passes over latitudes between 98.2°N and 98.2°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 35 share a similar altitude band with HORYU 2.
❓ Frequently Asked Questions
HORYU 2 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 595 km altitude. Its 98.2° 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 27,233 km/h.
HORYU 2 is operated by Kyushu Institute of Technology (KIT) (Japan). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 38340. You can track HORYU 2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
HORYU 2 was launched on 2012-05-17 from TNSTA. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks HORYU 2 (NORAD ID 38340) 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.
HORYU 2 travels at approximately 27,233 km/h (16,922 mph) — roughly 7.56 km/s. It completes 14.91 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.