Skip to content
Home Library Satellite Directory ATLAS CENTAUR R/B

ATLAS CENTAUR R/B

NORAD 43341 Rocket Body MEO 2018-036C
CONNECTING… MEO · NORAD 43341
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
31895 km
Apogee
35453 km
Inclination
6.7°
Period
1329.5 min
Mean Motion
1.08308719 rev/day
TLE Epoch
2026-06-25 12:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude33,674 km
Orbital Velocity11,358 km/h
Velocity3.15 km/s
Orbital Period22 hours 10 minutes
Orbits / Day1.08
Eccentricity0.0444
Semi-Major Axis40,045 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2018-04-14
Launch Site
Cape Canaveral, Florida
Int'l Designator
2018-036C
Object Type
Rocket Body
RCS Size
Medium (0.1–1 m²)
📖 About This Object
ATLAS CENTAUR R/B is a spent rocket body associated with United States, launched on 2018-04-14 from Cape Canaveral, Florida on the CBAS/EAGLE launch. It orbits in Medium Earth Orbit (MEO) at altitudes between 31,895 km and 35,453 km with an inclination of 6.7°. It travels at approximately 11,358 km/h (3.15 km/s), completing one full orbit every 22 hours 10 minutes — that’s roughly 1.08 orbits per day. 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 33,674 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 CENTAUR R/B’s average altitude, there are currently 0 active payloads and 2 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 6.7°, ATLAS CENTAUR R/B passes over latitudes between 6.7°N and 6.7°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. 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 CENTAUR R/B orbits in Medium Earth Orbit (MEO) at altitudes between 31,895 km (perigee) and 35,453 km (apogee), with an average altitude of approximately 33,674 km. It completes one orbit every 22 hours 10 minutes, travelling at approximately 11,358 km/h (7,057 mph).
ATLAS CENTAUR R/B (NORAD ID 43341) 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 2018-04-14 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 CENTAUR R/B (NORAD ID 43341) 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 11,358 km/h (7,057 mph) — roughly 3.15 km/s. It completes 1.08 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 2 sunrises and sunsets every 24 hours.