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SL-24 R/B

NORAD 40541 Rocket Body LEO 2015-014C
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
524 km
Apogee
1419 km
Inclination
97.3°
Period
104.5 min
Mean Motion
13.77817752 rev/day
TLE Epoch
2026-06-25 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude972 km
Orbital Velocity26,525 km/h
Velocity7.37 km/s
Orbital Period105 minutes
Orbits / Day13.78
Eccentricity0.0609
Semi-Major Axis7,343 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2015-03-25
Launch Site
OREN
Int'l Designator
2015-014C
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 2015-03-25 from OREN on the Kompsat-3A launch. After 11 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 524 km and 1,419 km with an inclination of 97.3°. It travels at approximately 26,525 km/h (7.37 km/s), completing one full orbit every 105 minutes — that’s roughly 13.78 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 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 972 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of SL-24 R/B’s average altitude, there are currently 314 active payloads and 987 tracked debris or rocket body fragments. With an inclination of 97.3°, SL-24 R/B passes over latitudes between 97.3°N and 97.3°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 163 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 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 972 km altitude. Its 97.3° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 105 minutes, travelling at 26,525 km/h.
SL-24 R/B (NORAD ID 40541) 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 2015-03-25 from OREN. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks SL-24 R/B (NORAD ID 40541) 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 26,525 km/h (16,482 mph) — roughly 7.37 km/s. It completes 13.78 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.