ATLAS 5 CENTAUR R/B
NORAD 32379
Rocket Body
MEO
2007-060B
CONNECTING…
MEO · NORAD 32379
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
296 km
Apogee
12784 km
Inclination
60.8°
Period
243.5 min
Mean Motion
5.91306820 rev/day
TLE Epoch
2026-06-25 16:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude6,540 km
Orbital Velocity20,003 km/h
Velocity5.56 km/s
Orbital Period4 hours 4 minutes
Orbits / Day5.91
Eccentricity0.4836
Semi-Major Axis12,911 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2007-12-10
Launch Site
Cape Canaveral, Florida
Int'l Designator
2007-060B
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 2007-12-10 from Cape Canaveral, Florida on the QUASAR 15? launch. After 19 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 296 km and 12,784 km with an inclination of 60.8°. It travels at approximately 20,003 km/h (5.56 km/s), completing one full orbit every 4 hours 4 minutes — that’s roughly 5.91 orbits per day. Its orbital eccentricity of 0.4836 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 6,540 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 6 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 60.8°, ATLAS 5 CENTAUR R/B passes over latitudes between 60.8°N and 60.8°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.
🔗 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 296 km (perigee) and 12,784 km (apogee), with an average altitude of approximately 6,540 km. It completes one orbit every 4 hours 4 minutes, travelling at approximately 20,003 km/h (12,429 mph).
ATLAS 5 CENTAUR R/B (NORAD ID 32379) 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 2007-12-10 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 ATLAS 5 CENTAUR R/B (NORAD ID 32379) 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 20,003 km/h (12,429 mph) — roughly 5.56 km/s. It completes 5.91 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 12 sunrises and sunsets every 24 hours.