SL-12 R/B(2)
NORAD 28512
Rocket Body
MEO
2004-053E
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
19051 km
Apogee
19174 km
Inclination
64.2°
Period
675.1 min
Mean Motion
2.13315276 rev/day
TLE Epoch
2026-06-26 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude19,113 km
Orbital Velocity14,238 km/h
Velocity3.95 km/s
Orbital Period11 hours 15 minutes
Orbits / Day2.13
Eccentricity0.0024
Semi-Major Axis25,484 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2004-12-26
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2004-053E
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
SL-12 R/B(2) is a spent rocket body associated with Russia (CIS), launched on 2004-12-26 from Baikonur, Kazakhstan on the Uragan No. 796 launch. With over 22 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 19,051 km and 19,174 km with an inclination of 64.2°. It travels at approximately 14,238 km/h (3.95 km/s), completing one full orbit every 11 hours 15 minutes — that’s roughly 2.13 orbits per day. Spent rocket bodies like SL-12 R/B(2) 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-12 R/B(2) orbits at an average altitude of 19,113 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-12 R/B(2)’s average altitude, there are currently 143 active payloads and 48 tracked debris or rocket body fragments — notable neighbours include COSMOS 1413 (GLONASS), COSMOS 1414 (GLONASS), COSMOS 1415 (GLONASS). With an inclination of 64.2°, SL-12 R/B(2) passes over latitudes between 64.2°N and 64.2°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. Russia (CIS) operates approximately 1,286 active satellites in total, of which 143 share a similar altitude band with SL-12 R/B(2).
🔗 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-12 R/B(2) orbits in Medium Earth Orbit (MEO) at altitudes between 19,051 km (perigee) and 19,174 km (apogee), with an average altitude of approximately 19,113 km. It completes one orbit every 11 hours 15 minutes, travelling at approximately 14,238 km/h (8,847 mph).
SL-12 R/B(2) (NORAD ID 28512) 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-12 R/B(2) was launched on 2004-12-26 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-12 R/B(2) (NORAD ID 28512) 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-12 R/B(2) travels at approximately 14,238 km/h (8,847 mph) — roughly 3.95 km/s. It completes 2.13 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.