EPSILON DEB
NORAD 39254
Debris
LEO
2013-049B
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LEO · NORAD 39254
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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
846 km
Apogee
1114 km
Inclination
29.7°
Period
104.7 min
Mean Motion
13.75476348 rev/day
TLE Epoch
2026-06-20 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude980 km
Orbital Velocity26,509 km/h
Velocity7.36 km/s
Orbital Period105 minutes
Orbits / Day13.75
Eccentricity0.0182
Semi-Major Axis7,351 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
2013-09-14
Launch Site
Uchinoura, Japan
Int'l Designator
2013-049B
Object Type
Debris
RCS Size
Large (>1 m²)
📖 About This Object
EPSILON DEB is a tracked piece of space debris attributed to Japan, launched on 2013-09-14 from Uchinoura, Japan on the SPRINT-A launch. After 13 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 846 km and 1,114 km with an inclination of 29.7°. It travels at approximately 26,509 km/h (7.36 km/s), completing one full orbit every 105 minutes — that’s roughly 13.75 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. As orbital debris, EPSILON 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
EPSILON DEB orbits at an average altitude of 980 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of EPSILON DEB’s average altitude, there are currently 281 active payloads and 946 tracked debris or rocket body fragments. With an inclination of 29.7°, EPSILON DEB passes over latitudes between 29.7°N and 29.7°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. Japan operates approximately 189 active satellites in total, of which 2 share a similar altitude band with EPSILON 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
EPSILON DEB orbits in Low Earth Orbit (LEO) at altitudes between 846 km (perigee) and 1,114 km (apogee), with an average altitude of approximately 980 km. It completes one orbit every 105 minutes, travelling at approximately 26,509 km/h (16,472 mph).
EPSILON DEB (NORAD ID 39254) 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.
EPSILON DEB was launched on 2013-09-14 from Uchinoura, Japan. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks EPSILON DEB (NORAD ID 39254) 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.
EPSILON DEB travels at approximately 26,509 km/h (16,472 mph) — roughly 7.36 km/s. It completes 13.75 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 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 7.36 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 EPSILON DEB. Read more about debris statistics and the Kessler syndrome.