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THOR AGENA B R/B

NORAD 1807 Rocket Body MEO 1965-098C
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Altitude (km)
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
501 km
Apogee
2613 km
Inclination
79.8°
Period
117.2 min
Mean Motion
12.28212252 rev/day
TLE Epoch
2026-09-16 02:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,557 km
Orbital Velocity25,526 km/h
Velocity7.09 km/s
Orbital Period117 minutes
Orbits / Day12.28
Eccentricity0.1332
Semi-Major Axis7,928 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
1965-098C
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 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 501 km and 2,613 km with an inclination of 79.8°. It travels at approximately 25,526 km/h (7.09 km/s), completing one full orbit every 117 minutes — that’s roughly 12.28 orbits per day. Its orbital eccentricity of 0.1332 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. 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 1,557 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 R/B’s average altitude, there are currently 50 active payloads and 352 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 79.8°, THOR AGENA B R/B 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 13,206 active satellites in total, of which 3 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 Medium Earth Orbit (MEO) at altitudes between 501 km (perigee) and 2,613 km (apogee), with an average altitude of approximately 1,557 km. It completes one orbit every 117 minutes, travelling at approximately 25,526 km/h (15,861 mph).
THOR AGENA B R/B (NORAD ID 1807) 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 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 R/B (NORAD ID 1807) 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 R/B travels at approximately 25,526 km/h (15,861 mph) — roughly 7.09 km/s. It completes 12.28 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 25 sunrises and sunsets every 24 hours.