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THOR DELTA 1 R/B

NORAD 5106 Rocket Body LEO 1971-024B
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
1352 km
Apogee
1421 km
Inclination
88.2°
Period
113.5 min
Mean Motion
12.68915745 rev/day
TLE Epoch
2026-09-16 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,387 km
Orbital Velocity25,805 km/h
Velocity7.17 km/s
Orbital Period113 minutes
Orbits / Day12.69
Eccentricity0.0044
Semi-Major Axis7,758 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1971-04-01
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1971-024B
Object Type
Rocket Body
RCS Size
Medium (0.1–1 m²)
📖 About This Object
THOR DELTA 1 R/B is a spent rocket body associated with United States, launched on 1971-04-01 from Vandenberg Space Force Base, United States on the Isis B launch. After more than 55 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 1,352 km and 1,421 km with an inclination of 88.2°. It travels at approximately 25,805 km/h (7.17 km/s), completing one full orbit every 113 minutes — that’s roughly 12.69 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. Spent rocket bodies like THOR DELTA 1 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 DELTA 1 R/B orbits at an average altitude of 1,387 km in the uppermost reaches of Low Earth Orbit. At this altitude, orbital decay is effectively zero without active deorbiting, and coverage footprints are significantly larger than lower LEO, though at the cost of higher latency. Within ±50 km of THOR DELTA 1 R/B’s average altitude, there are currently 253 active payloads and 243 tracked debris or rocket body fragments. With an inclination of 88.2°, THOR DELTA 1 R/B passes over latitudes between 88.2°N and 88.2°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, of which 12 share a similar altitude band with THOR DELTA 1 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 DELTA 1 R/B orbits in Low Earth Orbit (LEO) at altitudes between 1,352 km (perigee) and 1,421 km (apogee), with an average altitude of approximately 1,387 km. It completes one orbit every 113 minutes, travelling at approximately 25,805 km/h (16,035 mph).
THOR DELTA 1 R/B (NORAD ID 5106) 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 DELTA 1 R/B was launched on 1971-04-01 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 DELTA 1 R/B (NORAD ID 5106) 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 DELTA 1 R/B travels at approximately 25,805 km/h (16,035 mph) — roughly 7.17 km/s. It completes 12.69 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 25 sunrises and sunsets every 24 hours.