SL-8 R/B
NORAD 4391
Rocket Body
LEO
1970-036J
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
1468 km
Apogee
1588 km
Inclination
74.0°
Period
116.6 min
Mean Motion
12.34993814 rev/day
TLE Epoch
2026-09-16 02:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,528 km
Orbital Velocity25,573 km/h
Velocity7.10 km/s
Orbital Period117 minutes
Orbits / Day12.35
Eccentricity0.0076
Semi-Major Axis7,899 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1970-04-25
Launch Site
Plesetsk Cosmodrome, Russia
Int'l Designator
1970-036J
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 1970-04-25 from Plesetsk Cosmodrome, Russia on the Strela-1M launch. After more than 56 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 1,468 km and 1,588 km with an inclination of 74.0°. It travels at approximately 25,573 km/h (7.10 km/s), completing one full orbit every 117 minutes — that’s roughly 12.35 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of 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 1,528 km in the uppermost reaches of Low Earth Orbit. At this altitude, orbital decay is effectively zero without active deorbiting, and coverage footprints are significantly larger than lower LEO, though at the cost of higher latency. Within ±50 km of SL-8 R/B’s average altitude, there are currently 201 active payloads and 395 tracked debris or rocket body fragments. With an inclination of 74.0°, SL-8 R/B passes over latitudes between 74.0°N and 74.0°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 185 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 1,468 km (perigee) and 1,588 km (apogee), with an average altitude of approximately 1,528 km. It completes one orbit every 117 minutes, travelling at approximately 25,573 km/h (15,890 mph).
SL-8 R/B (NORAD ID 4391) 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 1970-04-25 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: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks SL-8 R/B (NORAD ID 4391) 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 25,573 km/h (15,890 mph) — roughly 7.10 km/s. It completes 12.35 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 25 sunrises and sunsets every 24 hours.