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ATLAS 5 CENTAUR R/B

NORAD 39071 Rocket Body MEO 2013-004B
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
4198 km
Apogee
34598 km
Inclination
25.1°
Period
686.4 min
Mean Motion
2.09790581 rev/day
TLE Epoch
2026-06-25 11:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude19,398 km
Orbital Velocity14,159 km/h
Velocity3.93 km/s
Orbital Period11 hours 26 minutes
Orbits / Day2.10
Eccentricity0.5899
Semi-Major Axis25,769 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2013-01-31
Launch Site
Cape Canaveral, Florida
Int'l Designator
2013-004B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
ATLAS 5 CENTAUR R/B is a spent rocket body associated with United States, launched on 2013-01-31 from Cape Canaveral, Florida on the TDRS K launch. After 13 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 4,198 km and 34,598 km with an inclination of 25.1°. It travels at approximately 14,159 km/h (3.93 km/s), completing one full orbit every 11 hours 26 minutes — that’s roughly 2.10 orbits per day. Its orbital eccentricity of 0.5899 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like ATLAS 5 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 5 CENTAUR R/B orbits at an average altitude of 19,398 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 ATLAS 5 CENTAUR R/B’s average altitude, there are currently 0 active payloads and 13 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 25.1°, ATLAS 5 CENTAUR R/B passes over latitudes between 25.1°N and 25.1°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
ATLAS 5 CENTAUR R/B orbits in Medium Earth Orbit (MEO) at altitudes between 4,198 km (perigee) and 34,598 km (apogee), with an average altitude of approximately 19,398 km. It completes one orbit every 11 hours 26 minutes, travelling at approximately 14,159 km/h (8,798 mph).
ATLAS 5 CENTAUR R/B (NORAD ID 39071) 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 5 CENTAUR R/B was launched on 2013-01-31 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 ATLAS 5 CENTAUR R/B (NORAD ID 39071) 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 5 CENTAUR R/B travels at approximately 14,159 km/h (8,798 mph) — roughly 3.93 km/s. It completes 2.10 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.