SL-24 R/B
NORAD 40047
Rocket Body
LEO
2014-033AP
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LEO · NORAD 40047
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
609 km
Apogee
1448 km
Inclination
97.9°
Period
105.7 min
Mean Motion
13.61965904 rev/day
TLE Epoch
2026-06-26 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,029 km
Orbital Velocity26,422 km/h
Velocity7.34 km/s
Orbital Period106 minutes
Orbits / Day13.62
Eccentricity0.0567
Semi-Major Axis7,400 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2014-06-19
Launch Site
OREN
Int'l Designator
2014-033AP
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
SL-24 R/B is a spent rocket body associated with Russia (CIS), launched on 2014-06-19 from OREN on the Dnepr Rideshare 9 launch. After 12 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 609 km and 1,448 km with an inclination of 97.9°. It travels at approximately 26,422 km/h (7.34 km/s), completing one full orbit every 106 minutes — that’s roughly 13.62 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 years. Spent rocket bodies like SL-24 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
SL-24 R/B orbits at an average altitude of 1,029 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 SL-24 R/B’s average altitude, there are currently 257 active payloads and 604 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0041. With an inclination of 97.9°, SL-24 R/B passes over latitudes between 97.9°N and 97.9°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. Russia (CIS) operates approximately 1,286 active satellites in total, of which 102 share a similar altitude band with SL-24 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
SL-24 R/B orbits in Low Earth Orbit (LEO) at altitudes between 609 km (perigee) and 1,448 km (apogee), with an average altitude of approximately 1,029 km. It completes one orbit every 106 minutes, travelling at approximately 26,422 km/h (16,418 mph).
SL-24 R/B (NORAD ID 40047) is a spent rocket body — the upper stage of a launch vehicle attributed to Russia (CIS). 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.
SL-24 R/B was launched on 2014-06-19 from OREN. At its current altitude, the estimated remaining orbital lifetime is: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks SL-24 R/B (NORAD ID 40047) 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.
SL-24 R/B travels at approximately 26,422 km/h (16,418 mph) — roughly 7.34 km/s. It completes 13.62 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 sunrises and sunsets every 24 hours.