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IUS R/B(1)

NORAD 20843 Rocket Body MEO 1990-090C
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
308 km
Apogee
27187 km
Inclination
28.4°
Period
473.6 min
Mean Motion
3.04067889 rev/day
TLE Epoch
2026-06-25 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude13,748 km
Orbital Velocity16,024 km/h
Velocity4.45 km/s
Orbital Period7 hours 54 minutes
Orbits / Day3.04
Eccentricity0.6680
Semi-Major Axis20,119 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1990-10-06
Launch Site
Cape Canaveral, Florida
Int'l Designator
1990-090C
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 1990-10-06 from Cape Canaveral, Florida on the OV-103 IUS deploy launch. With over 36 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 308 km and 27,187 km with an inclination of 28.4°. It travels at approximately 16,024 km/h (4.45 km/s), completing one full orbit every 7 hours 54 minutes — that’s roughly 3.04 orbits per day. Its orbital eccentricity of 0.6680 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 13,748 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 4 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 28.4°, IUS R/B(1) passes over latitudes between 28.4°N and 28.4°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 308 km (perigee) and 27,187 km (apogee), with an average altitude of approximately 13,748 km. It completes one orbit every 7 hours 54 minutes, travelling at approximately 16,024 km/h (9,957 mph).
IUS R/B(1) (NORAD ID 20843) 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 1990-10-06 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 20843) 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 16,024 km/h (9,957 mph) — roughly 4.45 km/s. It completes 3.04 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 6 sunrises and sunsets every 24 hours.