ATLAS CENTAUR 2 DEB
NORAD 19638
Debris
LEO
1963-047S
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LEO · NORAD 19638
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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
946 km
Apogee
1934 km
Inclination
31.0°
Period
114.7 min
Mean Motion
12.55845963 rev/day
TLE Epoch
2026-06-22 08:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,440 km
Orbital Velocity25,717 km/h
Velocity7.14 km/s
Orbital Period115 minutes
Orbits / Day12.56
Eccentricity0.0632
Semi-Major Axis7,811 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1963-11-27
Launch Site
Cape Canaveral, Florida
Int'l Designator
1963-047S
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, Florida 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 946 km and 1,934 km with an inclination of 31.0°. It travels at approximately 25,717 km/h (7.14 km/s), completing one full orbit every 115 minutes — that’s roughly 12.56 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of 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 1,440 km in the uppermost reaches of Low Earth Orbit. At this altitude, orbital decay is effectively zero without active deorbiting, and coverage footprints are significantly larger than lower LEO, though at the cost of higher latency. Within ±50 km of ATLAS CENTAUR 2 DEB’s average altitude, there are currently 377 active payloads and 191 tracked debris or rocket body fragments. With an inclination of 31.0°, ATLAS CENTAUR 2 DEB passes over latitudes between 31.0°N and 31.0°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 12,413 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 CENTAUR 2 DEB orbits in Low Earth Orbit (LEO) at altitudes between 946 km (perigee) and 1,934 km (apogee), with an average altitude of approximately 1,440 km. It completes one orbit every 115 minutes, travelling at approximately 25,717 km/h (15,980 mph).
ATLAS CENTAUR 2 DEB (NORAD ID 19638) 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, Florida, 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: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks ATLAS CENTAUR 2 DEB (NORAD ID 19638) 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 25,717 km/h (15,980 mph) — roughly 7.14 km/s. It completes 12.56 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 25 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 7.14 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.