SL-12 R/B(AUX MOTOR)
NORAD 15774
Rocket Body
LEO
1985-042F
CONNECTING…
LEO · NORAD 15774
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
785 km
Apogee
830 km
Inclination
66.6°
Period
101.0 min
Mean Motion
14.25384887 rev/day
TLE Epoch
2026-06-25 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude808 km
Orbital Velocity26,826 km/h
Velocity7.45 km/s
Orbital Period101 minutes
Orbits / Day14.25
Eccentricity0.0031
Semi-Major Axis7,179 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1985-05-30
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1985-042F
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 1985-05-30 from Baikonur, Kazakhstan on the Tselina-2 launch. With over 41 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 785 km and 830 km with an inclination of 66.6°. It travels at approximately 26,826 km/h (7.45 km/s), completing one full orbit every 101 minutes — that’s roughly 14.25 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. 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 808 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of SL-12 R/B(AUX MOTOR)’s average altitude, there are currently 438 active payloads and 2,334 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 66.6°, SL-12 R/B(AUX MOTOR) passes over latitudes between 66.6°N and 66.6°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 1,287 active satellites in total, of which 86 share a similar altitude band with SL-12 R/B(AUX MOTOR).
🔗 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 Low Earth Orbit (LEO) at altitudes between 785 km (perigee) and 830 km (apogee), with an average altitude of approximately 808 km. It completes one orbit every 101 minutes, travelling at approximately 26,826 km/h (16,669 mph).
SL-12 R/B(AUX MOTOR) (NORAD ID 15774) 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 1985-05-30 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: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks SL-12 R/B(AUX MOTOR) (NORAD ID 15774) 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 26,826 km/h (16,669 mph) — roughly 7.45 km/s. It completes 14.25 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.