THOR AGENA B R/B
NORAD 426
Rocket Body
LEO
1962-049B
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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
991 km
Apogee
1017 km
Inclination
80.5°
Period
105.2 min
Mean Motion
13.68771680 rev/day
TLE Epoch
2026-10-21 08:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,004 km
Orbital Velocity26,466 km/h
Velocity7.35 km/s
Orbital Period105 minutes
Orbits / Day13.69
Eccentricity0.0018
Semi-Major Axis7,375 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇺🇸 GSFC (United States)
Launch Date
1962-09-29
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1962-049B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
THOR AGENA B R/B is a spent rocket body associated with United States, launched on 1962-09-29 from Vandenberg Space Force Base, United States. After more than 64 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 991 km and 1,017 km with an inclination of 80.5°. It travels at approximately 26,466 km/h (7.35 km/s), completing one full orbit every 105 minutes — that’s roughly 13.69 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 years. Spent rocket bodies like THOR AGENA B R/B are among the largest pieces of uncontrolled space debris and are priority targets for collision avoidance manoeuvres and future active debris removal efforts.
🌍 Orbit Context
THOR AGENA B R/B orbits at an average altitude of 1,004 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 R/B’s average altitude, there are currently 289 active payloads and 1,052 tracked debris or rocket body fragments. With an inclination of 80.5°, THOR AGENA B R/B passes over latitudes between 80.5°N and 80.5°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. United States operates approximately 13,279 active satellites in total, of which 57 share a similar altitude band with THOR AGENA B R/B.
🔗 Spent Rocket Body
This is a spent rocket body — the upper stage of a launch vehicle that remains in orbit after delivering its payload. Rocket bodies are a significant contributor to the space debris population. Older stages often retained residual propellant that could later explode, creating debris fields. Modern guidelines require upper stages to either deorbit (controlled re-entry) or passivate (vent residual fuel) to reduce fragmentation risk. The FCC's 5-year deorbit rule and UN debris mitigation guidelines are increasingly enforced to address this growing problem.
❓ Frequently Asked Questions
THOR AGENA B R/B orbits in Low Earth Orbit (LEO) at altitudes between 991 km (perigee) and 1,017 km (apogee), with an average altitude of approximately 1,004 km. It completes one orbit every 105 minutes, travelling at approximately 26,466 km/h (16,445 mph).
THOR AGENA B R/B (NORAD ID 426) is a spent rocket body — the upper stage of a launch vehicle attributed to United States. It no longer serves a functional purpose but continues to orbit Earth as tracked debris. Spent upper stages are among the largest uncontrolled objects in orbit and are closely monitored for collision risk.
THOR AGENA B R/B was launched on 1962-09-29 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 R/B (NORAD ID 426) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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 R/B travels at approximately 26,466 km/h (16,445 mph) — roughly 7.35 km/s. It completes 13.69 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 sunrises and sunsets every 24 hours.