THOR AGENA B DEB
NORAD 2153
Debris
MEO
1965-098J
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MEO · NORAD 2153
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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
499 km
Apogee
2519 km
Inclination
79.8°
Period
116.2 min
Mean Motion
12.39416120 rev/day
TLE Epoch
2026-09-19 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,509 km
Orbital Velocity25,604 km/h
Velocity7.11 km/s
Orbital Period116 minutes
Orbits / Day12.39
Eccentricity0.1282
Semi-Major Axis7,880 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1965-11-29
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1965-098J
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
THOR AGENA B DEB is a tracked piece of space debris attributed to United States, launched on 1965-11-29 from Vandenberg Space Force Base, United States on the Alouette 2 launch. After more than 61 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Medium Earth Orbit (MEO) at altitudes between 499 km and 2,519 km with an inclination of 79.8°. It travels at approximately 25,604 km/h (7.11 km/s), completing one full orbit every 116 minutes — that’s roughly 12.39 orbits per day. Its orbital eccentricity of 0.1282 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. As orbital debris, THOR AGENA B 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
THOR AGENA B DEB orbits at an average altitude of 1,509 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 THOR AGENA B DEB’s average altitude, there are currently 286 active payloads and 395 tracked debris or rocket body fragments. With an inclination of 79.8°, THOR AGENA B DEB passes over latitudes between 79.8°N and 79.8°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. United States operates approximately 13,196 active satellites in total, of which 3 share a similar altitude band with THOR AGENA B 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
THOR AGENA B DEB orbits in Medium Earth Orbit (MEO) at altitudes between 499 km (perigee) and 2,519 km (apogee), with an average altitude of approximately 1,509 km. It completes one orbit every 116 minutes, travelling at approximately 25,604 km/h (15,910 mph).
THOR AGENA B DEB (NORAD ID 2153) 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 AGENA B DEB was launched on 1965-11-29 from Vandenberg Space Force Base, United States, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. At its current altitude, the estimated remaining orbital lifetime is: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks THOR AGENA B DEB (NORAD ID 2153) 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 AGENA B DEB travels at approximately 25,604 km/h (15,910 mph) — roughly 7.11 km/s. It completes 12.39 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 7.11 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 AGENA B DEB. Read more about debris statistics and the Kessler syndrome.