ATLAS CENTAUR 2 DEB
NORAD 701
Debris
LEO
1963-047G
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LEO · NORAD 701
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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
583 km
Apogee
1321 km
Inclination
30.0°
Period
104.1 min
Mean Motion
13.83477873 rev/day
TLE Epoch
2026-09-19 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude952 km
Orbital Velocity26,560 km/h
Velocity7.38 km/s
Orbital Period104 minutes
Orbits / Day13.83
Eccentricity0.0504
Semi-Major Axis7,323 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1963-11-27
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
1963-047G
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 583 km and 1,321 km with an inclination of 30.0°. It travels at approximately 26,560 km/h (7.38 km/s), completing one full orbit every 104 minutes — that’s roughly 13.83 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 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 952 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of ATLAS CENTAUR 2 DEB’s average altitude, there are currently 413 active payloads and 1,305 tracked debris or rocket body fragments. With an inclination of 30.0°, ATLAS CENTAUR 2 DEB passes over latitudes between 30.0°N and 30.0°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 13,199 active satellites in total, of which 146 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 583 km (perigee) and 1,321 km (apogee), with an average altitude of approximately 952 km. It completes one orbit every 104 minutes, travelling at approximately 26,560 km/h (16,504 mph).
ATLAS CENTAUR 2 DEB (NORAD ID 701) 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: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks ATLAS CENTAUR 2 DEB (NORAD ID 701) 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 26,560 km/h (16,504 mph) — roughly 7.38 km/s. It completes 13.83 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 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 7.38 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.