EPSILON R/B
NORAD 39255
Rocket Body
LEO
2013-049C
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LEO · NORAD 39255
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
806 km
Apogee
970 km
Inclination
29.8°
Period
102.7 min
Mean Motion
14.01646883 rev/day
TLE Epoch
2026-06-25 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude888 km
Orbital Velocity26,677 km/h
Velocity7.41 km/s
Orbital Period103 minutes
Orbits / Day14.02
Eccentricity0.0113
Semi-Major Axis7,259 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
2013-09-14
Launch Site
Uchinoura, Japan
Int'l Designator
2013-049C
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
EPSILON R/B is a spent rocket body associated with 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 806 km and 970 km with an inclination of 29.8°. It travels at approximately 26,677 km/h (7.41 km/s), completing one full orbit every 103 minutes — that’s roughly 14.02 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Spent rocket bodies like EPSILON R/B are among the largest pieces of uncontrolled space debris and are priority targets for collision avoidance manoeuvres and future active debris removal efforts.
🌍 Orbit Context
EPSILON R/B orbits at an average altitude of 888 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 R/B’s average altitude, there are currently 169 active payloads and 1,568 tracked debris or rocket body fragments. With an inclination of 29.8°, EPSILON R/B passes over latitudes between 29.8°N and 29.8°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 190 active satellites in total, of which 2 share a similar altitude band with EPSILON R/B.
🔗 Spent Rocket Body
This is a spent rocket body — the upper stage of a launch vehicle that remains in orbit after delivering its payload. Rocket bodies are a significant contributor to the space debris population. Older stages often retained residual propellant that could later explode, creating debris fields. Modern guidelines require upper stages to either deorbit (controlled re-entry) or passivate (vent residual fuel) to reduce fragmentation risk. The FCC's 5-year deorbit rule and UN debris mitigation guidelines are increasingly enforced to address this growing problem.
❓ Frequently Asked Questions
EPSILON R/B orbits in Low Earth Orbit (LEO) at altitudes between 806 km (perigee) and 970 km (apogee), with an average altitude of approximately 888 km. It completes one orbit every 103 minutes, travelling at approximately 26,677 km/h (16,576 mph).
EPSILON R/B (NORAD ID 39255) is a spent rocket body — the upper stage of a launch vehicle attributed to Japan. It no longer serves a functional purpose but continues to orbit Earth as tracked debris. Spent upper stages are among the largest uncontrolled objects in orbit and are closely monitored for collision risk.
EPSILON R/B 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 R/B (NORAD ID 39255) 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 R/B travels at approximately 26,677 km/h (16,576 mph) — roughly 7.41 km/s. It completes 14.02 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.