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IUS R/B(1)

NORAD 13971 Rocket Body MEO 1983-026D
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
285 km
Apogee
19452 km
Inclination
25.9°
Period
343.5 min
Mean Motion
4.19232630 rev/day
TLE Epoch
2026-06-25 09:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude9,869 km
Orbital Velocity17,835 km/h
Velocity4.95 km/s
Orbital Period5 hours 43 minutes
Orbits / Day4.19
Eccentricity0.5901
Semi-Major Axis16,240 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1983-04-04
Launch Site
Cape Canaveral, Florida
Int'l Designator
1983-026D
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
IUS R/B(1) is a spent rocket body associated with United States, launched on 1983-04-04 from Cape Canaveral, Florida on the OV-099 IUS deploy launch. With over 43 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 285 km and 19,452 km with an inclination of 25.9°. It travels at approximately 17,835 km/h (4.95 km/s), completing one full orbit every 5 hours 43 minutes — that’s roughly 4.19 orbits per day. Its orbital eccentricity of 0.5901 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like IUS R/B(1) 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
IUS R/B(1) orbits at an average altitude of 9,869 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of IUS R/B(1)’s average altitude, there are currently 0 active payloads and 7 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 25.9°, IUS R/B(1) passes over latitudes between 25.9°N and 25.9°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. United States operates approximately 12,413 active satellites in total.
🔗 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
IUS R/B(1) orbits in Medium Earth Orbit (MEO) at altitudes between 285 km (perigee) and 19,452 km (apogee), with an average altitude of approximately 9,869 km. It completes one orbit every 5 hours 43 minutes, travelling at approximately 17,835 km/h (11,082 mph).
IUS R/B(1) (NORAD ID 13971) is a spent rocket body — the upper stage of a launch vehicle attributed to United States. 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.
IUS R/B(1) was launched on 1983-04-04 from Cape Canaveral, Florida, one of the busiest launch facilities in the world, operated by NASA and the U.S. Space Force on Florida’s Atlantic coast. At its current altitude, the estimated remaining orbital lifetime is: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks IUS R/B(1) (NORAD ID 13971) 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.
IUS R/B(1) travels at approximately 17,835 km/h (11,082 mph) — roughly 4.95 km/s. It completes 4.19 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 8 sunrises and sunsets every 24 hours.