ATLAS 3B CENTAUR R/B
NORAD 28538
Rocket Body
LEO
2005-004B
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Latitude
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🛰️ Orbital Parameters
Perigee
937 km
Apogee
1256 km
Inclination
63.8°
Period
107.2 min
Mean Motion
13.43379980 rev/day
TLE Epoch
2026-06-25 15:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,097 km
Orbital Velocity26,302 km/h
Velocity7.31 km/s
Orbital Period107 minutes
Orbits / Day13.43
Eccentricity0.0214
Semi-Major Axis7,468 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2005-02-03
Launch Site
Cape Canaveral, Florida
Int'l Designator
2005-004B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
ATLAS 3B CENTAUR R/B is a spent rocket body associated with United States, launched on 2005-02-03 from Cape Canaveral, Florida on the INTRUDER 7 launch. With over 21 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 937 km and 1,256 km with an inclination of 63.8°. It travels at approximately 26,302 km/h (7.31 km/s), completing one full orbit every 107 minutes — that’s roughly 13.43 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 years. Spent rocket bodies like ATLAS 3B CENTAUR 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
ATLAS 3B CENTAUR R/B orbits at an average altitude of 1,097 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of ATLAS 3B CENTAUR R/B’s average altitude, there are currently 174 active payloads and 388 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0041. With an inclination of 63.8°, ATLAS 3B CENTAUR R/B passes over latitudes between 63.8°N and 63.8°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. United States operates approximately 12,413 active satellites in total, of which 12 share a similar altitude band with ATLAS 3B CENTAUR 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
ATLAS 3B CENTAUR R/B orbits in Low Earth Orbit (LEO) at altitudes between 937 km (perigee) and 1,256 km (apogee), with an average altitude of approximately 1,097 km. It completes one orbit every 107 minutes, travelling at approximately 26,302 km/h (16,343 mph).
ATLAS 3B CENTAUR R/B (NORAD ID 28538) 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.
ATLAS 3B CENTAUR R/B was launched on 2005-02-03 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: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks ATLAS 3B CENTAUR R/B (NORAD ID 28538) 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.
ATLAS 3B CENTAUR R/B travels at approximately 26,302 km/h (16,343 mph) — roughly 7.31 km/s. It completes 13.43 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 sunrises and sunsets every 24 hours.