ATLAS 5 CENTAUR DEB
NORAD 43976
Debris
MEO
2014-055AF
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MEO · NORAD 43976
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
8379 km
Apogee
35231 km
Inclination
19.9°
Period
784.8 min
Mean Motion
1.83492318 rev/day
TLE Epoch
2026-06-20 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude21,805 km
Orbital Velocity13,540 km/h
Velocity3.76 km/s
Orbital Period13 hours 5 minutes
Orbits / Day1.83
Eccentricity0.4765
Semi-Major Axis28,176 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2014-09-17
Launch Site
Cape Canaveral, Florida
Int'l Designator
2014-055AF
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
ATLAS 5 CENTAUR DEB is a tracked piece of space debris attributed to United States, launched on 2014-09-17 from Cape Canaveral, Florida on the CLIO launch. After 12 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 8,379 km and 35,231 km with an inclination of 19.9°. It travels at approximately 13,540 km/h (3.76 km/s), completing one full orbit every 13 hours 5 minutes — that’s roughly 1.83 orbits per day. Its orbital eccentricity of 0.4765 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. As orbital debris, ATLAS 5 CENTAUR DEB poses a potential collision risk to operational satellites in nearby orbits and is continuously monitored by the U.S. Space Surveillance Network and other tracking systems.
🌍 Orbit Context
ATLAS 5 CENTAUR DEB orbits at an average altitude of 21,805 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 DEB’s average altitude, there are currently 0 active payloads and 19 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 19.9°, ATLAS 5 CENTAUR DEB passes over latitudes between 19.9°N and 19.9°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. United States operates approximately 12,358 active satellites in total.
🔗 Tracked Space Debris
This is a tracked piece of orbital debris — a fragment from a collision, explosion, or separation event that no longer serves any useful purpose. Space surveillance networks catalogue objects larger than approximately 10 cm in LEO. Even small debris can be catastrophic at orbital velocities (7–8 km/s in LEO), carrying kinetic energy comparable to a hand grenade per centimetre-sized fragment. The growing debris population is one of the most pressing challenges for long-term space sustainability.
❓ Frequently Asked Questions
ATLAS 5 CENTAUR DEB orbits in Medium Earth Orbit (MEO) at altitudes between 8,379 km (perigee) and 35,231 km (apogee), with an average altitude of approximately 21,805 km. It completes one orbit every 13 hours 5 minutes, travelling at approximately 13,540 km/h (8,414 mph).
ATLAS 5 CENTAUR DEB (NORAD ID 43976) is a piece of tracked orbital debris attributed to United States. It was likely created by a fragmentation event, collision, or mission-related separation. Even small debris objects at orbital velocities carry enormous kinetic energy, so they are tracked by the U.S. Space Surveillance Network to enable collision avoidance for operational satellites.
ATLAS 5 CENTAUR DEB was launched on 2014-09-17 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 DEB (NORAD ID 43976) 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 DEB travels at approximately 13,540 km/h (8,414 mph) — roughly 3.76 km/s. It completes 1.83 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.
All tracked debris poses a potential collision risk to operational satellites. At orbital velocities, even a small object carries enormous kinetic energy — a 1 cm fragment at 3.76 km/s has the energy equivalent of a hand grenade. Space agencies perform routine conjunction assessments and may manoeuvre operational satellites to avoid tracked objects like ATLAS 5 CENTAUR DEB. Read more about debris statistics and the Kessler syndrome.