QAEM 100 R/B
NORAD 58818
Rocket Body
LEO
2024-015B
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LEO · NORAD 58818
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Altitude (km)
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Longitude
🛰️ Orbital Parameters
Perigee
717 km
Apogee
771 km
Inclination
64.5°
Period
99.7 min
Mean Motion
14.44302711 rev/day
TLE Epoch
2026-06-25 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude744 km
Orbital Velocity26,945 km/h
Velocity7.48 km/s
Orbital Period100 minutes
Orbits / Day14.44
Eccentricity0.0038
Semi-Major Axis7,115 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
Iran
Launch Date
2024-01-20
Launch Site
SMTS
Int'l Designator
2024-015B
Object Type
Rocket Body
RCS Size
Medium (0.1–1 m²)
📖 About This Object
QAEM 100 R/B is a spent rocket body associated with Iran, launched on 2024-01-20 from SMTS on the Suraya launch. It orbits in Low Earth Orbit (LEO) at altitudes between 717 km and 771 km with an inclination of 64.5°. 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 QAEM 100 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
QAEM 100 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 QAEM 100 R/B’s average altitude, there are currently 369 active payloads and 1,921 tracked debris or rocket body fragments — notable neighbours include LANDSAT 9. With an inclination of 64.5°, QAEM 100 R/B passes over latitudes between 64.5°N and 64.5°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. Iran operates approximately 5 active satellites in total.
🔗 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
QAEM 100 R/B orbits in Low Earth Orbit (LEO) at altitudes between 717 km (perigee) and 771 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).
QAEM 100 R/B (NORAD ID 58818) is a spent rocket body — the upper stage of a launch vehicle attributed to Iran. 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.
QAEM 100 R/B was launched on 2024-01-20 from SMTS. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks QAEM 100 R/B (NORAD ID 58818) 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.
QAEM 100 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.