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SL-23 R/B

NORAD 37835 Rocket Body MEO 2011-056B
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
5283 km
Apogee
35757 km
Inclination
19.6°
Period
731.7 min
Mean Motion
1.96794423 rev/day
TLE Epoch
2026-06-23 12:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude20,520 km
Orbital Velocity13,860 km/h
Velocity3.85 km/s
Orbital Period12 hours 12 minutes
Orbits / Day1.97
Eccentricity0.5666
Semi-Major Axis26,891 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2011-10-05
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2011-056B
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 2011-10-05 from Baikonur, Kazakhstan on the IS-18 launch. After 15 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 5,283 km and 35,757 km with an inclination of 19.6°. It travels at approximately 13,860 km/h (3.85 km/s), completing one full orbit every 12 hours 12 minutes — that’s roughly 1.97 orbits per day. Its orbital eccentricity of 0.5666 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 20,520 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. Within ±50 km of SL-23 R/B’s average altitude, there are currently 0 active payloads and 15 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 19.6°, SL-23 R/B passes over latitudes between 19.6°N and 19.6°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. 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 5,283 km (perigee) and 35,757 km (apogee), with an average altitude of approximately 20,520 km. It completes one orbit every 12 hours 12 minutes, travelling at approximately 13,860 km/h (8,612 mph).
SL-23 R/B (NORAD ID 37835) 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 2011-10-05 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 37835) 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 13,860 km/h (8,612 mph) — roughly 3.85 km/s. It completes 1.97 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.