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SL-12 R/B(AUX MOTOR)

NORAD 37143 Rocket Body MEO 2010-041G
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
284 km
Apogee
6614 km
Inclination
64.4°
Period
161.6 min
Mean Motion
8.91377775 rev/day
TLE Epoch
2026-07-16 11:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude3,449 km
Orbital Velocity22,936 km/h
Velocity6.37 km/s
Orbital Period2 hours 42 minutes
Orbits / Day8.91
Eccentricity0.3223
Semi-Major Axis9,820 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2010-09-02
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2010-041G
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 2010-09-02 from Baikonur, Kazakhstan on the Uragan-M No. 736 launch. After 16 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 284 km and 6,614 km with an inclination of 64.4°. It travels at approximately 22,936 km/h (6.37 km/s), completing one full orbit every 2 hours 42 minutes — that’s roughly 8.91 orbits per day. Its orbital eccentricity of 0.3223 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 3,449 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 64.4°, SL-12 R/B(AUX MOTOR) passes over latitudes between 64.4°N and 64.4°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 1,288 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 284 km (perigee) and 6,614 km (apogee), with an average altitude of approximately 3,449 km. It completes one orbit every 2 hours 42 minutes, travelling at approximately 22,936 km/h (14,252 mph).
SL-12 R/B(AUX MOTOR) (NORAD ID 37143) 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 2010-09-02 from Baikonur, 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 37143) 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(AUX MOTOR) travels at approximately 22,936 km/h (14,252 mph) — roughly 6.37 km/s. It completes 8.91 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 18 sunrises and sunsets every 24 hours.