SL-23 R/B
NORAD 39238
Rocket Body
MEO
2013-045B
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MEO · NORAD 39238
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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
2897 km
Apogee
35756 km
Inclination
26.4°
Period
683.6 min
Mean Motion
2.10661148 rev/day
TLE Epoch
2026-06-25 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude19,327 km
Orbital Velocity14,178 km/h
Velocity3.94 km/s
Orbital Period11 hours 24 minutes
Orbits / Day2.11
Eccentricity0.6393
Semi-Major Axis25,698 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2013-08-31
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2013-045B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
SL-23 R/B is a spent rocket body associated with Russia (CIS), launched on 2013-08-31 from Baikonur, Kazakhstan on the Amos 4 launch. After 13 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 2,897 km and 35,756 km with an inclination of 26.4°. It travels at approximately 14,178 km/h (3.94 km/s), completing one full orbit every 11 hours 24 minutes — that’s roughly 2.11 orbits per day. Its orbital eccentricity of 0.6393 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like SL-23 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-23 R/B orbits at an average altitude of 19,327 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. With an inclination of 26.4°, SL-23 R/B passes over latitudes between 26.4°N and 26.4°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. Russia (CIS) operates approximately 1,286 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
SL-23 R/B orbits in Medium Earth Orbit (MEO) at altitudes between 2,897 km (perigee) and 35,756 km (apogee), with an average altitude of approximately 19,327 km. It completes one orbit every 11 hours 24 minutes, travelling at approximately 14,178 km/h (8,810 mph).
SL-23 R/B (NORAD ID 39238) 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-23 R/B was launched on 2013-08-31 from Baikonur, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. View the full satellite launch log.
Yes — Orbital Radar tracks SL-23 R/B (NORAD ID 39238) 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-23 R/B travels at approximately 14,178 km/h (8,810 mph) — roughly 3.94 km/s. It completes 2.11 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.