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ATLAS 5 CENTAUR R/B

NORAD 44483 Rocket Body MEO 2019-051C
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
13770 km
Apogee
35395 km
Inclination
7.2°
Period
903.6 min
Mean Motion
1.59360084 rev/day
TLE Epoch
2026-06-25 10:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude24,583 km
Orbital Velocity12,919 km/h
Velocity3.59 km/s
Orbital Period15 hours 4 minutes
Orbits / Day1.59
Eccentricity0.3493
Semi-Major Axis30,954 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2019-08-08
Launch Site
Cape Canaveral, Florida
Int'l Designator
2019-051C
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 2019-08-08 from Cape Canaveral, Florida on the AEHF 5 launch. It orbits in Medium Earth Orbit (MEO) at altitudes between 13,770 km and 35,395 km with an inclination of 7.2°. It travels at approximately 12,919 km/h (3.59 km/s), completing one full orbit every 15 hours 4 minutes — that’s roughly 1.59 orbits per day. Its orbital eccentricity of 0.3493 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 24,583 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 7.2°, ATLAS 5 CENTAUR R/B passes over latitudes between 7.2°N and 7.2°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 13,770 km (perigee) and 35,395 km (apogee), with an average altitude of approximately 24,583 km. It completes one orbit every 15 hours 4 minutes, travelling at approximately 12,919 km/h (8,027 mph).
ATLAS 5 CENTAUR R/B (NORAD ID 44483) 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 2019-08-08 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 44483) 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 12,919 km/h (8,027 mph) — roughly 3.59 km/s. It completes 1.59 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 3 sunrises and sunsets every 24 hours.