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ATLAS H R/B

NORAD 17998 Rocket Body LEO 1987-043B
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🛰️ Orbital Parameters
Perigee
548 km
Apogee
1585 km
Inclination
63.3°
Period
106.5 min
Mean Motion
13.51573257 rev/day
TLE Epoch
2026-10-15 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,067 km
Orbital Velocity26,355 km/h
Velocity7.32 km/s
Orbital Period107 minutes
Orbits / Day13.52
Eccentricity0.0697
Semi-Major Axis7,438 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇺🇸 NRL (United States)
Launch Date
1987-05-15
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1987-043B
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 1987-05-15 from Vandenberg Space Force Base, United States on the PARCAE 9 launch. With over 39 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 548 km and 1,585 km with an inclination of 63.3°. It travels at approximately 26,355 km/h (7.32 km/s), completing one full orbit every 107 minutes — that’s roughly 13.52 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 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 1,067 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 309 active payloads and 589 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0041. 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 13,201 active satellites in total, of which 41 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 548 km (perigee) and 1,585 km (apogee), with an average altitude of approximately 1,067 km. It completes one orbit every 107 minutes, travelling at approximately 26,355 km/h (16,376 mph).
ATLAS H R/B (NORAD ID 17998) 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 1987-05-15 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: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks ATLAS H R/B (NORAD ID 17998) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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 26,355 km/h (16,376 mph) — roughly 7.32 km/s. It completes 13.52 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 sunrises and sunsets every 24 hours.