SL-12 R/B(AUX MOTOR)
NORAD 4789
Rocket Body
MEO
1970-103B
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MEO · NORAD 4789
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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
1585 km
Apogee
5087 km
Inclination
51.6°
Period
158.8 min
Mean Motion
9.06813819 rev/day
TLE Epoch
2026-09-15 09:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude3,336 km
Orbital Velocity23,069 km/h
Velocity6.41 km/s
Orbital Period2 hours 39 minutes
Orbits / Day9.07
Eccentricity0.1804
Semi-Major Axis9,707 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1970-12-02
Launch Site
Baikonur Cosmodrome, Kazakhstan
Int'l Designator
1970-103B
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 1970-12-02 from Baikonur Cosmodrome, Kazakhstan on the L-1e No. 2K launch. After more than 56 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 1,585 km and 5,087 km with an inclination of 51.6°. It travels at approximately 23,069 km/h (6.41 km/s), completing one full orbit every 2 hours 39 minutes — that’s roughly 9.07 orbits per day. Its orbital eccentricity of 0.1804 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 3,336 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 51.6°, SL-12 R/B(AUX MOTOR) passes over latitudes between 51.6°N and 51.6°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 1,537 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 1,585 km (perigee) and 5,087 km (apogee), with an average altitude of approximately 3,336 km. It completes one orbit every 2 hours 39 minutes, travelling at approximately 23,069 km/h (14,334 mph).
SL-12 R/B(AUX MOTOR) (NORAD ID 4789) 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 1970-12-02 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 4789) 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 23,069 km/h (14,334 mph) — roughly 6.41 km/s. It completes 9.07 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 18 sunrises and sunsets every 24 hours.