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QAEM 100 R/B

NORAD 61071 Rocket Body LEO 2024-165A
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
474 km
Apogee
568 km
Inclination
64.1°
Period
95.0 min
Mean Motion
15.15006727 rev/day
TLE Epoch
2026-06-26 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude521 km
Orbital Velocity27,378 km/h
Velocity7.60 km/s
Orbital Period95 minutes
Orbits / Day15.15
Eccentricity0.0068
Semi-Major Axis6,892 km
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
Iran
Launch Date
2024-09-14
Launch Site
SMTS
Int'l Designator
2024-165A
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
QAEM 100 R/B is a spent rocket body associated with Iran, launched on 2024-09-14 from SMTS on the Chamran-1 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 474 km and 568 km with an inclination of 64.1°. It travels at approximately 27,378 km/h (7.60 km/s), completing one full orbit every 95 minutes — that’s roughly 15.15 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 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 521 km in the core of Low Earth Orbit, the most heavily utilised altitude band. The balance of moderate drag (limiting debris accumulation) and short signal path (enabling low-latency links and high-resolution imaging) makes this regime the default for most commercial and government missions. Within ±50 km of QAEM 100 R/B’s average altitude, there are currently 7,288 active payloads and 272 tracked debris or rocket body fragments — notable neighbours include STARLINK-1184, STARLINK-1231, STARLINK-1276. This makes it one of the more crowded altitude bands, containing roughly 41.7% of all active satellites. With an inclination of 64.1°, QAEM 100 R/B passes over latitudes between 64.1°N and 64.1°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, of which 2 share a similar altitude band with QAEM 100 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
QAEM 100 R/B orbits in Low Earth Orbit (LEO) at altitudes between 474 km (perigee) and 568 km (apogee), with an average altitude of approximately 521 km. It completes one orbit every 95 minutes, travelling at approximately 27,378 km/h (17,012 mph).
QAEM 100 R/B (NORAD ID 61071) 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 2024-09-14 from SMTS. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks QAEM 100 R/B (NORAD ID 61071) 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 27,378 km/h (17,012 mph) — roughly 7.60 km/s. It completes 15.15 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.