ATLAS 5 CENTAUR R/B
NORAD 36396
Rocket Body
MEO
2010-005B
CONNECTING…
MEO · NORAD 36396
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
2508 km
Apogee
33384 km
Inclination
28.6°
Period
629.3 min
Mean Motion
2.28842798 rev/day
TLE Epoch
2026-06-26 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude17,946 km
Orbital Velocity14,575 km/h
Velocity4.05 km/s
Orbital Period10 hours 29 minutes
Orbits / Day2.29
Eccentricity0.6349
Semi-Major Axis24,317 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2010-02-11
Launch Site
Cape Canaveral, Florida
Int'l Designator
2010-005B
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 2010-02-11 from Cape Canaveral, Florida on the SDO launch. After 16 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 2,508 km and 33,384 km with an inclination of 28.6°. It travels at approximately 14,575 km/h (4.05 km/s), completing one full orbit every 10 hours 29 minutes — that’s roughly 2.29 orbits per day. Its orbital eccentricity of 0.6349 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 17,946 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 14 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 28.6°, ATLAS 5 CENTAUR R/B passes over latitudes between 28.6°N and 28.6°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 2,508 km (perigee) and 33,384 km (apogee), with an average altitude of approximately 17,946 km. It completes one orbit every 10 hours 29 minutes, travelling at approximately 14,575 km/h (9,057 mph).
ATLAS 5 CENTAUR R/B (NORAD ID 36396) 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 2010-02-11 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 36396) 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 14,575 km/h (9,057 mph) — roughly 4.05 km/s. It completes 2.29 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 5 sunrises and sunsets every 24 hours.