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ATLAS CENTAUR R/B

NORAD 6155 Rocket Body LEO 1972-065B
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
612 km
Apogee
659 km
Inclination
35.0°
Period
97.4 min
Mean Motion
14.78045992 rev/day
TLE Epoch
2026-09-16 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude636 km
Orbital Velocity27,153 km/h
Velocity7.54 km/s
Orbital Period97 minutes
Orbits / Day14.78
Eccentricity0.0034
Semi-Major Axis7,007 km
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1972-08-21
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
1972-065B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
ATLAS CENTAUR R/B is a spent rocket body associated with United States, launched on 1972-08-21 from Cape Canaveral Space Force Station, United States on the OAO-C launch. After more than 54 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Low Earth Orbit (LEO) at altitudes between 612 km and 659 km with an inclination of 35.0°. It travels at approximately 27,153 km/h (7.54 km/s), completing one full orbit every 97 minutes — that’s roughly 14.78 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 years. Spent rocket bodies like ATLAS 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 CENTAUR R/B orbits at an average altitude of 636 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of ATLAS CENTAUR R/B’s average altitude, there are currently 982 active payloads and 961 tracked debris or rocket body fragments — notable neighbours include AQUA, ONEWEB-0050. This makes it one of the more crowded altitude bands, containing roughly 5.3% of all active satellites. With an inclination of 35.0°, ATLAS CENTAUR R/B passes over latitudes between 35.0°N and 35.0°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 13,206 active satellites in total, of which 514 share a similar altitude band with ATLAS 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 CENTAUR R/B orbits in Low Earth Orbit (LEO) at altitudes between 612 km (perigee) and 659 km (apogee), with an average altitude of approximately 636 km. It completes one orbit every 97 minutes, travelling at approximately 27,153 km/h (16,872 mph).
ATLAS CENTAUR R/B (NORAD ID 6155) 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 CENTAUR R/B was launched on 1972-08-21 from Cape Canaveral Space Force Station, United States, 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: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks ATLAS CENTAUR R/B (NORAD ID 6155) 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 CENTAUR R/B travels at approximately 27,153 km/h (16,872 mph) — roughly 7.54 km/s. It completes 14.78 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.