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ATLAS CENTAUR 2 DEB

NORAD 3741 Debris LEO 1963-047L
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
568 km
Apogee
901 km
Inclination
29.9°
Period
99.5 min
Mean Motion
14.47346950 rev/day
TLE Epoch
2026-09-19 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude735 km
Orbital Velocity26,963 km/h
Velocity7.49 km/s
Orbital Period99 minutes
Orbits / Day14.47
Eccentricity0.0234
Semi-Major Axis7,106 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1963-11-27
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
1963-047L
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
ATLAS CENTAUR 2 DEB is a tracked piece of space debris attributed to United States, launched on 1963-11-27 from Cape Canaveral Space Force Station, United States on the AC-2 launch. After more than 63 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Low Earth Orbit (LEO) at altitudes between 568 km and 901 km with an inclination of 29.9°. It travels at approximately 26,963 km/h (7.49 km/s), completing one full orbit every 99 minutes — that’s roughly 14.47 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. As orbital debris, ATLAS CENTAUR 2 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 CENTAUR 2 DEB orbits at an average altitude of 735 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of ATLAS CENTAUR 2 DEB’s average altitude, there are currently 401 active payloads and 2,021 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, ONEWEB-0179. With an inclination of 29.9°, ATLAS CENTAUR 2 DEB passes over latitudes between 29.9°N and 29.9°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 13,199 active satellites in total, of which 168 share a similar altitude band with ATLAS CENTAUR 2 DEB.
🔗 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 CENTAUR 2 DEB orbits in Low Earth Orbit (LEO) at altitudes between 568 km (perigee) and 901 km (apogee), with an average altitude of approximately 735 km. It completes one orbit every 99 minutes, travelling at approximately 26,963 km/h (16,754 mph).
ATLAS CENTAUR 2 DEB (NORAD ID 3741) 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 CENTAUR 2 DEB was launched on 1963-11-27 from Cape Canaveral Space Force Station, United States, one of the busiest launch facilities in the world, operated by NASA and the U.S. Space Force on Florida’s Atlantic coast. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks ATLAS CENTAUR 2 DEB (NORAD ID 3741) 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 2 DEB travels at approximately 26,963 km/h (16,754 mph) — roughly 7.49 km/s. It completes 14.47 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 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 7.49 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 CENTAUR 2 DEB. Read more about debris statistics and the Kessler syndrome.