N-1 DEB
NORAD 13132
Debris
LEO
1978-018C
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LEO · NORAD 13132
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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
972 km
Apogee
1284 km
Inclination
69.2°
Period
107.9 min
Mean Motion
13.34989032 rev/day
TLE Epoch
2026-06-19 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,128 km
Orbital Velocity26,246 km/h
Velocity7.29 km/s
Orbital Period108 minutes
Orbits / Day13.35
Eccentricity0.0208
Semi-Major Axis7,499 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
1978-02-16
Launch Site
TNSTA
Int'l Designator
1978-018C
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
N-1 DEB is a tracked piece of space debris attributed to 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 972 km and 1,284 km with an inclination of 69.2°. It travels at approximately 26,246 km/h (7.29 km/s), completing one full orbit every 108 minutes — that’s roughly 13.35 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 years. As orbital debris, N-1 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
N-1 DEB orbits at an average altitude of 1,128 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 DEB’s average altitude, there are currently 285 active payloads and 353 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0250, ONEWEB-0527, ONEWEB-0528. With an inclination of 69.2°, N-1 DEB passes over latitudes between 69.2°N and 69.2°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. Japan operates approximately 189 active satellites in total.
🔗 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
N-1 DEB orbits in Low Earth Orbit (LEO) at altitudes between 972 km (perigee) and 1,284 km (apogee), with an average altitude of approximately 1,128 km. It completes one orbit every 108 minutes, travelling at approximately 26,246 km/h (16,309 mph).
N-1 DEB (NORAD ID 13132) 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.
N-1 DEB 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 DEB (NORAD ID 13132) 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 DEB travels at approximately 26,246 km/h (16,309 mph) — roughly 7.29 km/s. It completes 13.35 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 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 7.29 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 N-1 DEB. Read more about debris statistics and the Kessler syndrome.