M-4S R/B
NORAD 5498
Rocket Body
LEO
1971-080B
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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
867 km
Apogee
1748 km
Inclination
32.0°
Period
111.8 min
Mean Motion
12.88511538 rev/day
TLE Epoch
2026-09-15 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,308 km
Orbital Velocity25,938 km/h
Velocity7.20 km/s
Orbital Period112 minutes
Orbits / Day12.89
Eccentricity0.0574
Semi-Major Axis7,679 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
1971-09-28
Launch Site
Uchinoura Space Center, Japan
Int'l Designator
1971-080B
Object Type
Rocket Body
RCS Size
Medium (0.1–1 m²)
📖 About This Object
M-4S R/B is a spent rocket body associated with Japan, launched on 1971-09-28 from Uchinoura Space Center, Japan on the MS-F2 launch. After more than 55 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 867 km and 1,748 km with an inclination of 32.0°. It travels at approximately 25,938 km/h (7.20 km/s), completing one full orbit every 112 minutes — that’s roughly 12.89 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. Spent rocket bodies like M-4S 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
M-4S R/B orbits at an average altitude of 1,308 km in the uppermost reaches of Low Earth Orbit. At this altitude, orbital decay is effectively zero without active deorbiting, and coverage footprints are significantly larger than lower LEO, though at the cost of higher latency. Within ±50 km of M-4S R/B’s average altitude, there are currently 20 active payloads and 381 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 32.0°, M-4S R/B passes over latitudes between 32.0°N and 32.0°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 2 share a similar altitude band with M-4S 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
M-4S R/B orbits in Low Earth Orbit (LEO) at altitudes between 867 km (perigee) and 1,748 km (apogee), with an average altitude of approximately 1,308 km. It completes one orbit every 112 minutes, travelling at approximately 25,938 km/h (16,117 mph).
M-4S R/B (NORAD ID 5498) 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.
M-4S R/B was launched on 1971-09-28 from Uchinoura Space Center, Japan. At its current altitude, the estimated remaining orbital lifetime is: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks M-4S R/B (NORAD ID 5498) 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.
M-4S R/B travels at approximately 25,938 km/h (16,117 mph) — roughly 7.20 km/s. It completes 12.89 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 26 sunrises and sunsets every 24 hours.