Skip to content
Home Library Satellite Directory N-1 R/B

N-1 R/B

NORAD 10675 Rocket Body LEO 1978-018B
CONNECTING… LEO · NORAD 10675
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
973 km
Apogee
1209 km
Inclination
69.4°
Period
107.1 min
Mean Motion
13.44894129 rev/day
TLE Epoch
2026-06-25 12:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,091 km
Orbital Velocity26,311 km/h
Velocity7.31 km/s
Orbital Period107 minutes
Orbits / Day13.45
Eccentricity0.0158
Semi-Major Axis7,462 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
1978-02-16
Launch Site
TNSTA
Int'l Designator
1978-018B
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 1978-02-16 from TNSTA on the ISS-b launch. With over 48 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 973 km and 1,209 km with an inclination of 69.4°. It travels at approximately 26,311 km/h (7.31 km/s), completing one full orbit every 107 minutes — that’s roughly 13.45 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 1,091 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 182 active payloads and 397 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0041. With an inclination of 69.4°, N-1 R/B passes over latitudes between 69.4°N and 69.4°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. Japan operates approximately 190 active satellites in total, of which 3 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 973 km (perigee) and 1,209 km (apogee), with an average altitude of approximately 1,091 km. It completes one orbit every 107 minutes, travelling at approximately 26,311 km/h (16,349 mph).
N-1 R/B (NORAD ID 10675) 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 1978-02-16 from TNSTA. 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 10675) 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 26,311 km/h (16,349 mph) — roughly 7.31 km/s. It completes 13.45 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 sunrises and sunsets every 24 hours.