H-2A DEB
NORAD 38347
Debris
LEO
2012-025H
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LEO · NORAD 38347
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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
582 km
Apogee
593 km
Inclination
98.2°
Period
96.4 min
Mean Motion
14.93397722 rev/day
TLE Epoch
2026-06-20 09:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude588 km
Orbital Velocity27,247 km/h
Velocity7.57 km/s
Orbital Period96 minutes
Orbits / Day14.93
Eccentricity0.0008
Semi-Major Axis6,959 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
2012-05-17
Launch Site
TNSTA
Int'l Designator
2012-025H
Object Type
Debris
RCS Size
Large (>1 m²)
📖 About This Object
H-2A DEB is a tracked piece of space debris attributed to Japan, launched on 2012-05-17 from TNSTA on the GCOM-W1 launch. After 14 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 582 km and 593 km with an inclination of 98.2°. It travels at approximately 27,247 km/h (7.57 km/s), completing one full orbit every 96 minutes — that’s roughly 14.93 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. As orbital debris, H-2A DEB poses a potential collision risk to operational satellites in nearby orbits and is continuously monitored by the U.S. Space Surveillance Network and other tracking systems.
🌍 Orbit Context
H-2A DEB orbits at an average altitude of 588 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 H-2A DEB’s average altitude, there are currently 3,172 active payloads and 586 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 18.2% of all active satellites. With an inclination of 98.2°, H-2A DEB 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 38 share a similar altitude band with H-2A DEB.
🔗 Tracked Space Debris
This is a tracked piece of orbital debris — a fragment from a collision, explosion, or separation event that no longer serves any useful purpose. Space surveillance networks catalogue objects larger than approximately 10 cm in LEO. Even small debris can be catastrophic at orbital velocities (7–8 km/s in LEO), carrying kinetic energy comparable to a hand grenade per centimetre-sized fragment. The growing debris population is one of the most pressing challenges for long-term space sustainability.
❓ Frequently Asked Questions
H-2A DEB is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 588 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 96 minutes, travelling at 27,247 km/h.
H-2A DEB (NORAD ID 38347) is a piece of tracked orbital debris attributed to Japan. It was likely created by a fragmentation event, collision, or mission-related separation. Even small debris objects at orbital velocities carry enormous kinetic energy, so they are tracked by the U.S. Space Surveillance Network to enable collision avoidance for operational satellites.
H-2A DEB 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 H-2A DEB (NORAD ID 38347) 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.
H-2A DEB travels at approximately 27,247 km/h (16,930 mph) — roughly 7.57 km/s. It completes 14.93 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.
All tracked debris poses a potential collision risk to operational satellites. At orbital velocities, even a small object carries enormous kinetic energy — a 1 cm fragment at 7.57 km/s has the energy equivalent of a hand grenade. Space agencies perform routine conjunction assessments and may manoeuvre operational satellites to avoid tracked objects like H-2A DEB. Read more about debris statistics and the Kessler syndrome.