IUS R/B(1)
NORAD 21806
Rocket Body
MEO
1991-080C
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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
396 km
Apogee
34108 km
Inclination
26.4°
Period
602.5 min
Mean Motion
2.38998531 rev/day
TLE Epoch
2026-06-24 08:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude17,252 km
Orbital Velocity14,788 km/h
Velocity4.11 km/s
Orbital Period10 hours 3 minutes
Orbits / Day2.39
Eccentricity0.7135
Semi-Major Axis23,623 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1991-11-24
Launch Site
Cape Canaveral, Florida
Int'l Designator
1991-080C
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 1991-11-24 from Cape Canaveral, Florida on the OV-104 IUS deploy launch. With over 35 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 396 km and 34,108 km with an inclination of 26.4°. It travels at approximately 14,788 km/h (4.11 km/s), completing one full orbit every 10 hours 3 minutes — that’s roughly 2.39 orbits per day. Its orbital eccentricity of 0.7135 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 17,252 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 9 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 26.4°, IUS R/B(1) passes over latitudes between 26.4°N and 26.4°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 396 km (perigee) and 34,108 km (apogee), with an average altitude of approximately 17,252 km. It completes one orbit every 10 hours 3 minutes, travelling at approximately 14,788 km/h (9,189 mph).
IUS R/B(1) (NORAD ID 21806) 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 1991-11-24 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 21806) 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 14,788 km/h (9,189 mph) — roughly 4.11 km/s. It completes 2.39 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 5 sunrises and sunsets every 24 hours.