SL-12 R/B(AUX MOTOR)
NORAD 28632
Rocket Body
MEO
2005-010D
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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
282 km
Apogee
11550 km
Inclination
47.3°
Period
226.1 min
Mean Motion
6.36910257 rev/day
TLE Epoch
2026-10-15 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude5,916 km
Orbital Velocity20,504 km/h
Velocity5.70 km/s
Orbital Period3 hours 46 minutes
Orbits / Day6.37
Eccentricity0.4585
Semi-Major Axis12,287 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2005-03-29
Launch Site
Baikonur Cosmodrome, Kazakhstan
Int'l Designator
2005-010D
Object Type
Rocket Body
RCS Size
Medium (0.1–1 m²)
📖 About This Object
SL-12 R/B(AUX MOTOR) is a spent rocket body associated with Russia (CIS), launched on 2005-03-29 from Baikonur Cosmodrome, Kazakhstan on the Ekspress AM-2 launch. With over 21 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 282 km and 11,550 km with an inclination of 47.3°. It travels at approximately 20,504 km/h (5.70 km/s), completing one full orbit every 3 hours 46 minutes — that’s roughly 6.37 orbits per day. Its orbital eccentricity of 0.4585 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like SL-12 R/B(AUX MOTOR) 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(AUX MOTOR) orbits at an average altitude of 5,916 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(AUX MOTOR)’s average altitude, there are currently 3 active payloads and 4 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 47.3°, SL-12 R/B(AUX MOTOR) passes over latitudes between 47.3°N and 47.3°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 1,514 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-12 R/B(AUX MOTOR) orbits in Medium Earth Orbit (MEO) at altitudes between 282 km (perigee) and 11,550 km (apogee), with an average altitude of approximately 5,916 km. It completes one orbit every 3 hours 46 minutes, travelling at approximately 20,504 km/h (12,741 mph).
SL-12 R/B(AUX MOTOR) (NORAD ID 28632) 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(AUX MOTOR) was launched on 2005-03-29 from Baikonur Cosmodrome, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. At its current altitude, the estimated remaining orbital lifetime is: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks SL-12 R/B(AUX MOTOR) (NORAD ID 28632) 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-12 R/B(AUX MOTOR) travels at approximately 20,504 km/h (12,741 mph) — roughly 5.70 km/s. It completes 6.37 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 13 sunrises and sunsets every 24 hours.