ATLAS 5 CENTAUR R/B
NORAD 40888
Rocket Body
MEO
2015-044B
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MEO · NORAD 40888
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🛰️ Orbital Parameters
Perigee
3781 km
Apogee
35181 km
Inclination
19.3°
Period
689.7 min
Mean Motion
2.08777887 rev/day
TLE Epoch
2026-06-25 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude19,481 km
Orbital Velocity14,136 km/h
Velocity3.93 km/s
Orbital Period11 hours 30 minutes
Orbits / Day2.09
Eccentricity0.6073
Semi-Major Axis25,852 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2015-09-02
Launch Site
Cape Canaveral, Florida
Int'l Designator
2015-044B
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 2015-09-02 from Cape Canaveral, Florida on the MUOS 4 launch. After 11 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 3,781 km and 35,181 km with an inclination of 19.3°. It travels at approximately 14,136 km/h (3.93 km/s), completing one full orbit every 11 hours 30 minutes — that’s roughly 2.09 orbits per day. Its orbital eccentricity of 0.6073 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 19,481 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. With an inclination of 19.3°, ATLAS 5 CENTAUR R/B passes over latitudes between 19.3°N and 19.3°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 5 CENTAUR R/B orbits in Medium Earth Orbit (MEO) at altitudes between 3,781 km (perigee) and 35,181 km (apogee), with an average altitude of approximately 19,481 km. It completes one orbit every 11 hours 30 minutes, travelling at approximately 14,136 km/h (8,784 mph).
ATLAS 5 CENTAUR R/B (NORAD ID 40888) 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 2015-09-02 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 40888) 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 14,136 km/h (8,784 mph) — roughly 3.93 km/s. It completes 2.09 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.