MINOTAUR R/B
NORAD 26066
Rocket Body
LEO
2000-004F
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LEO · NORAD 26066
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
739 km
Apogee
785 km
Inclination
100.2°
Period
100.1 min
Mean Motion
14.39015378 rev/day
TLE Epoch
2026-06-25 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude762 km
Orbital Velocity26,911 km/h
Velocity7.48 km/s
Orbital Period100 minutes
Orbits / Day14.39
Eccentricity0.0032
Semi-Major Axis7,133 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2000-01-27
Launch Site
Vandenberg SFB, California
Int'l Designator
2000-004F
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
MINOTAUR R/B is a spent rocket body associated with United States, launched on 2000-01-27 from Vandenberg SFB, California on the JAWSAT launch. With over 26 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 739 km and 785 km with an inclination of 100.2°. It travels at approximately 26,911 km/h (7.48 km/s), completing one full orbit every 100 minutes — that’s roughly 14.39 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. Spent rocket bodies like MINOTAUR 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
MINOTAUR R/B orbits at an average altitude of 762 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of MINOTAUR R/B’s average altitude, there are currently 367 active payloads and 2,070 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0179. With an inclination of 100.2°, MINOTAUR R/B passes over latitudes between 100.2°N and 100.2°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 12,413 active satellites in total, of which 151 share a similar altitude band with MINOTAUR 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
MINOTAUR R/B orbits in Low Earth Orbit (LEO) at altitudes between 739 km (perigee) and 785 km (apogee), with an average altitude of approximately 762 km. It completes one orbit every 100 minutes, travelling at approximately 26,911 km/h (16,722 mph).
MINOTAUR R/B (NORAD ID 26066) 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.
MINOTAUR R/B was launched on 2000-01-27 from Vandenberg SFB, California, 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: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks MINOTAUR R/B (NORAD ID 26066) 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.
MINOTAUR R/B travels at approximately 26,911 km/h (16,722 mph) — roughly 7.48 km/s. It completes 14.39 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.