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IUS R/B(2)

NORAD 23438 Rocket Body GEO 1994-084D
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
35514 km
Apogee
35552 km
Inclination
14.3°
Period
1423.1 min
Mean Motion
1.01177143 rev/day
TLE Epoch
2026-06-25 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,533 km
Orbital Velocity11,103 km/h
Velocity3.08 km/s
Orbital Period23 hours 43 minutes
Orbits / Day1.01
Eccentricity0.0005
Semi-Major Axis41,904 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1994-12-22
Launch Site
Cape Canaveral, Florida
Int'l Designator
1994-084D
Object Type
Rocket Body
RCS Size
Unknown
📖 About This Object
IUS R/B(2) is a spent rocket body associated with United States, launched on 1994-12-22 from Cape Canaveral, Florida on the DSP 17 launch. With over 32 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,514 km and 35,552 km with an inclination of 14.3°. It travels at approximately 11,103 km/h (3.08 km/s), completing one full orbit every 23 hours 43 minutes — that’s roughly 1.01 orbits per day. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Spent rocket bodies like IUS R/B(2) 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(2) occupies geostationary orbit at approximately 35,786 km above the equator, where its orbital period matches the Earth’s 24-hour rotation. From the ground, it appears to hover over a fixed point — ideal for broadcast television, weather monitoring and wideband communications. With an inclination of 14.3°, it traces a small figure-of-eight pattern relative to the equator rather than remaining perfectly stationary, which can indicate aging stationkeeping fuel or a deliberate inclined-orbit strategy. Within ±50 km of IUS R/B(2)’s average altitude, there are currently 1 active payload and 37 tracked debris or rocket body fragments. 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(2) orbits at approximately 35,533 km altitude, where the orbital period matches the Earth’s 24-hour rotation. This means it stays above the same point on the equator at all times. Its actual speed is still 11,103 km/h — it just keeps pace with the ground below. With an inclination of 14.3°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
IUS R/B(2) (NORAD ID 23438) 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(2) was launched on 1994-12-22 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. View the full satellite launch log.
Yes — Orbital Radar tracks IUS R/B(2) (NORAD ID 23438) 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(2) travels at approximately 11,103 km/h (6,899 mph) — roughly 3.08 km/s. Despite this high speed, it appears stationary from the ground because it matches the Earth’s rotation. Geostationary satellites are actually slower than LEO satellites because orbital velocity decreases with altitude.