ATLAS 5 CENTAUR DEB
NORAD 44015
Debris
MEO
2014-055BW
CONNECTING…
MEO · NORAD 44015
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
6938 km
Apogee
34405 km
Inclination
21.2°
Period
737.9 min
Mean Motion
1.95145873 rev/day
TLE Epoch
2026-06-16 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude20,672 km
Orbital Velocity13,821 km/h
Velocity3.84 km/s
Orbital Period12 hours 18 minutes
Orbits / Day1.95
Eccentricity0.5078
Semi-Major Axis27,043 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
2014-055BW
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 6,938 km and 34,405 km with an inclination of 21.2°. It travels at approximately 13,821 km/h (3.84 km/s), completing one full orbit every 12 hours 18 minutes — that’s roughly 1.95 orbits per day. Its orbital eccentricity of 0.5078 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 20,672 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 1 active payload and 6 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 21.2°, ATLAS 5 CENTAUR DEB passes over latitudes between 21.2°N and 21.2°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 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 6,938 km (perigee) and 34,405 km (apogee), with an average altitude of approximately 20,672 km. It completes one orbit every 12 hours 18 minutes, travelling at approximately 13,821 km/h (8,588 mph).
ATLAS 5 CENTAUR DEB (NORAD ID 44015) 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 44015) 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 13,821 km/h (8,588 mph) — roughly 3.84 km/s. It completes 1.95 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 3.84 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.