SL-12 R/B(AUX MOTOR)
NORAD 7400
Rocket Body
MEO
1974-060E
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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
1768 km
Apogee
30773 km
Inclination
44.8°
Period
565.4 min
Mean Motion
2.54706196 rev/day
TLE Epoch
2026-09-16 02:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude16,271 km
Orbital Velocity15,105 km/h
Velocity4.20 km/s
Orbital Period9 hours 25 minutes
Orbits / Day2.55
Eccentricity0.6405
Semi-Major Axis22,642 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1974-07-29
Launch Site
Baikonur Cosmodrome, Kazakhstan
Int'l Designator
1974-060E
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 1974-07-29 from Baikonur Cosmodrome, Kazakhstan on the Molniya-1 11F658 No. 38 launch. After more than 52 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Medium Earth Orbit (MEO) at altitudes between 1,768 km and 30,773 km with an inclination of 44.8°. It travels at approximately 15,105 km/h (4.20 km/s), completing one full orbit every 9 hours 25 minutes — that’s roughly 2.55 orbits per day. Its orbital eccentricity of 0.6405 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 16,271 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 0 active payloads and 7 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 44.8°, SL-12 R/B(AUX MOTOR) passes over latitudes between 44.8°N and 44.8°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 1,537 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 1,768 km (perigee) and 30,773 km (apogee), with an average altitude of approximately 16,271 km. It completes one orbit every 9 hours 25 minutes, travelling at approximately 15,105 km/h (9,386 mph).
SL-12 R/B(AUX MOTOR) (NORAD ID 7400) 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 1974-07-29 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 7400) 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 15,105 km/h (9,386 mph) — roughly 4.20 km/s. It completes 2.55 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 5 sunrises and sunsets every 24 hours.