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THOR ABLE DEB (YO)

NORAD 115 Debris LEO 1960-002D
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
553 km
Apogee
590 km
Inclination
48.2°
Period
96.1 min
Mean Motion
14.98594370 rev/day
TLE Epoch
2026-09-17 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude572 km
Orbital Velocity27,278 km/h
Velocity7.58 km/s
Orbital Period96 minutes
Orbits / Day14.99
Eccentricity0.0027
Semi-Major Axis6,943 km
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1960-04-01
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
1960-002D
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
THOR ABLE DEB (YO) is a tracked piece of space debris attributed to United States, launched on 1960-04-01 from Cape Canaveral Space Force Station, United States. After more than 66 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 553 km and 590 km with an inclination of 48.2°. It travels at approximately 27,278 km/h (7.58 km/s), completing one full orbit every 96 minutes — that’s roughly 14.99 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 years. As orbital debris, THOR ABLE DEB (YO) 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
THOR ABLE DEB (YO) orbits at an average altitude of 572 km in the core of Low Earth Orbit, the most heavily utilised altitude band. The balance of moderate drag (limiting debris accumulation) and short signal path (enabling low-latency links and high-resolution imaging) makes this regime the default for most commercial and government missions. Within ±50 km of THOR ABLE DEB (YO)’s average altitude, there are currently 1,441 active payloads and 532 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3005, STARLINK-3090. This makes it one of the more crowded altitude bands, containing roughly 7.7% of all active satellites. With an inclination of 48.2°, THOR ABLE DEB (YO) passes over latitudes between 48.2°N and 48.2°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 13,195 active satellites in total, of which 860 share a similar altitude band with THOR ABLE DEB (YO).
🔗 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
THOR ABLE DEB (YO) orbits in Low Earth Orbit (LEO) at altitudes between 553 km (perigee) and 590 km (apogee), with an average altitude of approximately 572 km. It completes one orbit every 96 minutes, travelling at approximately 27,278 km/h (16,950 mph).
THOR ABLE DEB (YO) (NORAD ID 115) 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.
THOR ABLE DEB (YO) was launched on 1960-04-01 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: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks THOR ABLE DEB (YO) (NORAD ID 115) 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.
THOR ABLE DEB (YO) travels at approximately 27,278 km/h (16,950 mph) — roughly 7.58 km/s. It completes 14.99 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 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 7.58 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 THOR ABLE DEB (YO). Read more about debris statistics and the Kessler syndrome.