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ATLAS 28E R/B

NORAD 20563 Rocket Body LEO 1990-031D
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Altitude (km)
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
586 km
Apogee
670 km
Inclination
89.9°
Period
97.3 min
Mean Motion
14.80391992 rev/day
TLE Epoch
2026-06-26 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude628 km
Orbital Velocity27,168 km/h
Velocity7.55 km/s
Orbital Period97 minutes
Orbits / Day14.80
Eccentricity0.0060
Semi-Major Axis6,999 km
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1990-04-11
Launch Site
Vandenberg SFB, California
Int'l Designator
1990-031D
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
ATLAS 28E R/B is a spent rocket body associated with United States, launched on 1990-04-11 from Vandenberg SFB, California on the POGS launch. With over 36 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 586 km and 670 km with an inclination of 89.9°. It travels at approximately 27,168 km/h (7.55 km/s), completing one full orbit every 97 minutes — that’s roughly 14.80 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 years. Spent rocket bodies like ATLAS 28E 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 28E R/B orbits at an average altitude of 628 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 28E R/B’s average altitude, there are currently 799 active payloads and 828 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-5823, STARLINK-34374. With an inclination of 89.9°, ATLAS 28E R/B passes over latitudes between 89.9°N and 89.9°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 349 share a similar altitude band with ATLAS 28E 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 28E R/B orbits in Low Earth Orbit (LEO) at altitudes between 586 km (perigee) and 670 km (apogee), with an average altitude of approximately 628 km. It completes one orbit every 97 minutes, travelling at approximately 27,168 km/h (16,881 mph).
ATLAS 28E R/B (NORAD ID 20563) 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 28E R/B was launched on 1990-04-11 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: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks ATLAS 28E R/B (NORAD ID 20563) 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 28E R/B travels at approximately 27,168 km/h (16,881 mph) — roughly 7.55 km/s. It completes 14.80 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.