ATLAS H R/B
NORAD 16592
Rocket Body
LEO
1986-014B
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
766 km
Apogee
1200 km
Inclination
63.3°
Period
104.8 min
Mean Motion
13.74573817 rev/day
TLE Epoch
2026-06-25 09:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude983 km
Orbital Velocity26,504 km/h
Velocity7.36 km/s
Orbital Period105 minutes
Orbits / Day13.75
Eccentricity0.0295
Semi-Major Axis7,354 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1986-02-09
Launch Site
Vandenberg SFB, California
Int'l Designator
1986-014B
Object Type
Rocket Body
RCS Size
Medium (0.1–1 m²)
📖 About This Object
ATLAS H R/B is a spent rocket body associated with United States, launched on 1986-02-09 from Vandenberg SFB, California on the PARCAE 8 launch. With over 40 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 766 km and 1,200 km with an inclination of 63.3°. It travels at approximately 26,504 km/h (7.36 km/s), completing one full orbit every 105 minutes — that’s roughly 13.75 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Spent rocket bodies like ATLAS H 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 H R/B orbits at an average altitude of 983 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of ATLAS H R/B’s average altitude, there are currently 300 active payloads and 942 tracked debris or rocket body fragments. With an inclination of 63.3°, ATLAS H R/B passes over latitudes between 63.3°N and 63.3°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 88 share a similar altitude band with ATLAS H 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 H R/B orbits in Low Earth Orbit (LEO) at altitudes between 766 km (perigee) and 1,200 km (apogee), with an average altitude of approximately 983 km. It completes one orbit every 105 minutes, travelling at approximately 26,504 km/h (16,469 mph).
ATLAS H R/B (NORAD ID 16592) 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 H R/B was launched on 1986-02-09 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: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks ATLAS H R/B (NORAD ID 16592) 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 H R/B travels at approximately 26,504 km/h (16,469 mph) — roughly 7.36 km/s. It completes 13.75 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 sunrises and sunsets every 24 hours.