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THOR AGENA B DEB

NORAD 1951 Debris LEO 1965-098G
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
474 km
Apogee
1604 km
Inclination
79.6°
Period
106.0 min
Mean Motion
13.59126314 rev/day
TLE Epoch
2026-09-19 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,039 km
Orbital Velocity26,404 km/h
Velocity7.33 km/s
Orbital Period106 minutes
Orbits / Day13.59
Eccentricity0.0762
Semi-Major Axis7,410 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1965-11-29
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1965-098G
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 Low Earth Orbit (LEO) at altitudes between 474 km and 1,604 km with an inclination of 79.6°. It travels at approximately 26,404 km/h (7.33 km/s), completing one full orbit every 106 minutes — that’s roughly 13.59 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 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 1,039 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 THOR AGENA B DEB’s average altitude, there are currently 323 active payloads and 698 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0041. With an inclination of 79.6°, THOR AGENA B DEB passes over latitudes between 79.6°N and 79.6°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 40 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 Low Earth Orbit (LEO) at altitudes between 474 km (perigee) and 1,604 km (apogee), with an average altitude of approximately 1,039 km. It completes one orbit every 106 minutes, travelling at approximately 26,404 km/h (16,406 mph).
THOR AGENA B DEB (NORAD ID 1951) 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: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks THOR AGENA B DEB (NORAD ID 1951) 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 26,404 km/h (16,406 mph) — roughly 7.33 km/s. It completes 13.59 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 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 7.33 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.