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ATLAS V CENTAUR R/B

NORAD 41329 Rocket Body MEO 2016-007B
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
20685 km
Apogee
21285 km
Inclination
55.7°
Period
750.8 min
Mean Motion
1.91799466 rev/day
TLE Epoch
2026-06-25 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude20,985 km
Orbital Velocity13,742 km/h
Velocity3.82 km/s
Orbital Period12 hours 31 minutes
Orbits / Day1.92
Eccentricity0.0110
Semi-Major Axis27,356 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2016-02-05
Launch Site
Cape Canaveral, Florida
Int'l Designator
2016-007B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
ATLAS V CENTAUR R/B is a spent rocket body associated with United States, launched on 2016-02-05 from Cape Canaveral, Florida on the GPS SVN 70 launch. After 10 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 20,685 km and 21,285 km with an inclination of 55.7°. It travels at approximately 13,742 km/h (3.82 km/s), completing one full orbit every 12 hours 31 minutes — that’s roughly 1.92 orbits per day. Spent rocket bodies like ATLAS V 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 V CENTAUR R/B orbits at an average altitude of 20,985 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 V CENTAUR R/B’s average altitude, there are currently 6 active payloads and 11 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 55.7°, ATLAS V CENTAUR R/B passes over latitudes between 55.7°N and 55.7°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 5 share a similar altitude band with ATLAS V 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 V CENTAUR R/B orbits in Medium Earth Orbit (MEO) at altitudes between 20,685 km (perigee) and 21,285 km (apogee), with an average altitude of approximately 20,985 km. It completes one orbit every 12 hours 31 minutes, travelling at approximately 13,742 km/h (8,539 mph).
ATLAS V CENTAUR R/B (NORAD ID 41329) 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 V CENTAUR R/B was launched on 2016-02-05 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 V CENTAUR R/B (NORAD ID 41329) 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 V CENTAUR R/B travels at approximately 13,742 km/h (8,539 mph) — roughly 3.82 km/s. It completes 1.92 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.