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THOR AGENA D R/B

NORAD 2255 Rocket Body MEO 1966-056B
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Altitude (km)
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
4178 km
Apogee
4279 km
Inclination
87.0°
Period
181.2 min
Mean Motion
7.94755978 rev/day
TLE Epoch
2026-09-16 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude4,229 km
Orbital Velocity22,076 km/h
Velocity6.13 km/s
Orbital Period3 hours 1 minutes
Orbits / Day7.95
Eccentricity0.0048
Semi-Major Axis10,600 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1966-06-24
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1966-056B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
THOR AGENA D R/B is a spent rocket body associated with United States, launched on 1966-06-24 from Vandenberg Space Force Base, United States on the Pageos A launch. After more than 60 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 4,178 km and 4,279 km with an inclination of 87.0°. It travels at approximately 22,076 km/h (6.13 km/s), completing one full orbit every 3 hours 1 minutes — that’s roughly 7.95 orbits per day. Spent rocket bodies like THOR AGENA D 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 D R/B orbits at an average altitude of 4,229 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 D R/B’s average altitude, there are currently 0 active payloads and 3 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 87.0°, THOR AGENA D R/B passes over latitudes between 87.0°N and 87.0°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 13,206 active satellites in total.
🔗 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 D R/B orbits in Medium Earth Orbit (MEO) at altitudes between 4,178 km (perigee) and 4,279 km (apogee), with an average altitude of approximately 4,229 km. It completes one orbit every 3 hours 1 minutes, travelling at approximately 22,076 km/h (13,718 mph).
THOR AGENA D R/B (NORAD ID 2255) 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 D R/B was launched on 1966-06-24 from Vandenberg Space Force Base, United States, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. View the full satellite launch log.
Yes — Orbital Radar tracks THOR AGENA D R/B (NORAD ID 2255) 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 D R/B travels at approximately 22,076 km/h (13,718 mph) — roughly 6.13 km/s. It completes 7.95 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 16 sunrises and sunsets every 24 hours.