N-1 R/B
NORAD 8352
Rocket Body
LEO
1975-082B
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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
969 km
Apogee
1094 km
Inclination
47.0°
Period
105.8 min
Mean Motion
13.61119063 rev/day
TLE Epoch
2026-09-16 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,032 km
Orbital Velocity26,417 km/h
Velocity7.34 km/s
Orbital Period106 minutes
Orbits / Day13.61
Eccentricity0.0084
Semi-Major Axis7,403 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
1975-09-09
Launch Site
Tanegashima Space Center, Japan
Int'l Designator
1975-082B
Object Type
Rocket Body
RCS Size
Medium (0.1–1 m²)
📖 About This Object
N-1 R/B is a spent rocket body associated with Japan, launched on 1975-09-09 from Tanegashima Space Center, Japan on the ETS 1 launch. After more than 51 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Low Earth Orbit (LEO) at altitudes between 969 km and 1,094 km with an inclination of 47.0°. It travels at approximately 26,417 km/h (7.34 km/s), completing one full orbit every 106 minutes — that’s roughly 13.61 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 years. Spent rocket bodies like N-1 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
N-1 R/B orbits at an average altitude of 1,032 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 N-1 R/B’s average altitude, there are currently 359 active payloads and 762 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0041. With an inclination of 47.0°, N-1 R/B passes over latitudes between 47.0°N and 47.0°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 208 active satellites in total, of which 7 share a similar altitude band with N-1 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
N-1 R/B orbits in Low Earth Orbit (LEO) at altitudes between 969 km (perigee) and 1,094 km (apogee), with an average altitude of approximately 1,032 km. It completes one orbit every 106 minutes, travelling at approximately 26,417 km/h (16,415 mph).
N-1 R/B (NORAD ID 8352) 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.
N-1 R/B was launched on 1975-09-09 from Tanegashima Space Center, Japan, Japan’s primary launch site, operated by JAXA on a small island south of Kyushu. At its current altitude, the estimated remaining orbital lifetime is: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks N-1 R/B (NORAD ID 8352) 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.
N-1 R/B travels at approximately 26,417 km/h (16,415 mph) — roughly 7.34 km/s. It completes 13.61 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 sunrises and sunsets every 24 hours.