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MINOTAUR 1 R/B

NORAD 48849 Rocket Body LEO 2021-052D
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Longitude
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🛰️ Orbital Parameters
Perigee
569 km
Apogee
575 km
Inclination
55.0°
Period
96.1 min
Mean Motion
14.98357402 rev/day
TLE Epoch
2026-06-26 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude572 km
Orbital Velocity27,277 km/h
Velocity7.58 km/s
Orbital Period96 minutes
Orbits / Day14.98
Eccentricity0.0004
Semi-Major Axis6,943 km
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2021-06-15
Launch Site
Wallops Island, Virginia
Int'l Designator
2021-052D
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
MINOTAUR 1 R/B is a spent rocket body associated with United States, launched on 2021-06-15 from Wallops Island, Virginia on the NROL-111 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 569 km and 575 km with an inclination of 55.0°. It travels at approximately 27,277 km/h (7.58 km/s), completing one full orbit every 96 minutes — that’s roughly 14.98 orbits per day. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 years. Spent rocket bodies like MINOTAUR 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
MINOTAUR 1 R/B orbits at an average altitude of 572 km in the core of Low Earth Orbit, the most heavily utilised altitude band. The balance of moderate drag (limiting debris accumulation) and short signal path (enabling low-latency links and high-resolution imaging) makes this regime the default for most commercial and government missions. Within ±50 km of MINOTAUR 1 R/B’s average altitude, there are currently 2,971 active payloads and 500 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-1522, STARLINK-2112. This makes it one of the more crowded altitude bands, containing roughly 17% of all active satellites. With an inclination of 55.0°, MINOTAUR 1 R/B passes over latitudes between 55.0°N and 55.0°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 12,413 active satellites in total, of which 2,441 share a similar altitude band with MINOTAUR 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
MINOTAUR 1 R/B orbits in Low Earth Orbit (LEO) at altitudes between 569 km (perigee) and 575 km (apogee), with an average altitude of approximately 572 km. It completes one orbit every 96 minutes, travelling at approximately 27,277 km/h (16,949 mph).
MINOTAUR 1 R/B (NORAD ID 48849) 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 1 R/B was launched on 2021-06-15 from Wallops Island, Virginia. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks MINOTAUR 1 R/B (NORAD ID 48849) 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 1 R/B travels at approximately 27,277 km/h (16,949 mph) — roughly 7.58 km/s. It completes 14.98 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.