SL-8 R/B
NORAD 5051
Rocket Body
LEO
1971-020B
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
946 km
Apogee
1009 km
Inclination
65.8°
Period
104.6 min
Mean Motion
13.76128756 rev/day
TLE Epoch
2026-09-15 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude978 km
Orbital Velocity26,514 km/h
Velocity7.36 km/s
Orbital Period105 minutes
Orbits / Day13.76
Eccentricity0.0043
Semi-Major Axis7,349 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1971-03-18
Launch Site
Plesetsk Cosmodrome, Russia
Int'l Designator
1971-020B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
SL-8 R/B is a spent rocket body associated with Russia (CIS), launched on 1971-03-18 from Plesetsk Cosmodrome, Russia on the DS-P1-M No. 3 launch. After more than 55 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Low Earth Orbit (LEO) at altitudes between 946 km and 1,009 km with an inclination of 65.8°. It travels at approximately 26,514 km/h (7.36 km/s), completing one full orbit every 105 minutes — that’s roughly 13.76 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Spent rocket bodies like SL-8 R/B 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-8 R/B orbits at an average altitude of 978 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-8 R/B’s average altitude, there are currently 369 active payloads and 1,179 tracked debris or rocket body fragments. With an inclination of 65.8°, SL-8 R/B passes over latitudes between 65.8°N and 65.8°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, of which 200 share a similar altitude band with SL-8 R/B.
🔗 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-8 R/B orbits in Low Earth Orbit (LEO) at altitudes between 946 km (perigee) and 1,009 km (apogee), with an average altitude of approximately 978 km. It completes one orbit every 105 minutes, travelling at approximately 26,514 km/h (16,475 mph).
SL-8 R/B (NORAD ID 5051) 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-8 R/B was launched on 1971-03-18 from Plesetsk Cosmodrome, Russia, Russia’s northern military cosmodrome, used primarily for high-inclination and polar orbit launches. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks SL-8 R/B (NORAD ID 5051) 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-8 R/B travels at approximately 26,514 km/h (16,475 mph) — roughly 7.36 km/s. It completes 13.76 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.