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ATLAS 41E R/B

NORAD 15596 Rocket Body LEO 1985-021B
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
720 km
Apogee
768 km
Inclination
108.0°
Period
99.7 min
Mean Motion
14.44435333 rev/day
TLE Epoch
2026-06-25 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude744 km
Orbital Velocity26,945 km/h
Velocity7.48 km/s
Orbital Period100 minutes
Orbits / Day14.44
Eccentricity0.0034
Semi-Major Axis7,115 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1985-03-13
Launch Site
Vandenberg SFB, California
Int'l Designator
1985-021B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
ATLAS 41E R/B is a spent rocket body associated with United States, launched on 1985-03-13 from Vandenberg SFB, California on the Geosat launch. With over 41 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 720 km and 768 km with an inclination of 108.0°. It travels at approximately 26,945 km/h (7.48 km/s), completing one full orbit every 100 minutes — that’s roughly 14.44 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. Spent rocket bodies like ATLAS 41E 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
ATLAS 41E R/B orbits at an average altitude of 744 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 ATLAS 41E R/B’s average altitude, there are currently 369 active payloads and 1,924 tracked debris or rocket body fragments — notable neighbours include LANDSAT 9. With an inclination of 108.0°, ATLAS 41E R/B passes over latitudes between 108.0°N and 108.0°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 12,413 active satellites in total, of which 145 share a similar altitude band with ATLAS 41E 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
ATLAS 41E R/B orbits in Low Earth Orbit (LEO) at altitudes between 720 km (perigee) and 768 km (apogee), with an average altitude of approximately 744 km. It completes one orbit every 100 minutes, travelling at approximately 26,945 km/h (16,743 mph).
ATLAS 41E R/B (NORAD ID 15596) 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.
ATLAS 41E R/B was launched on 1985-03-13 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 ATLAS 41E R/B (NORAD ID 15596) 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.
ATLAS 41E R/B travels at approximately 26,945 km/h (16,743 mph) — roughly 7.48 km/s. It completes 14.44 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.