SL-24 R/B
NORAD 39228
Rocket Body
LEO
2013-042B
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LEO · NORAD 39228
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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
539 km
Apogee
1187 km
Inclination
97.5°
Period
102.2 min
Mean Motion
14.08851469 rev/day
TLE Epoch
2026-10-14 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude863 km
Orbital Velocity26,723 km/h
Velocity7.42 km/s
Orbital Period102 minutes
Orbits / Day14.09
Eccentricity0.0448
Semi-Major Axis7,234 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2013-08-22
Launch Site
Yasny / Dombarovsky, Russia
Int'l Designator
2013-042B
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 2013-08-22 from Yasny / Dombarovsky, Russia on the Kompsat-5 launch. After 13 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 539 km and 1,187 km with an inclination of 97.5°. It travels at approximately 26,723 km/h (7.42 km/s), completing one full orbit every 102 minutes — that’s roughly 14.09 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 863 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 258 active payloads and 2,147 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0455. With an inclination of 97.5°, SL-24 R/B passes over latitudes between 97.5°N and 97.5°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 1,514 active satellites in total, of which 74 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 863 km altitude. Its 97.5° 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 102 minutes, travelling at 26,723 km/h.
SL-24 R/B (NORAD ID 39228) 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 2013-08-22 from Yasny / Dombarovsky, Russia. 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 39228) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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 26,723 km/h (16,605 mph) — roughly 7.42 km/s. It completes 14.09 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.