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SL-8 R/B

NORAD 4255 Rocket Body LEO 1969-103B
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Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
1140 km
Apogee
1156 km
Inclination
74.0°
Period
108.3 min
Mean Motion
13.29657408 rev/day
TLE Epoch
2026-09-16 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,148 km
Orbital Velocity26,211 km/h
Velocity7.28 km/s
Orbital Period108 minutes
Orbits / Day13.30
Eccentricity0.0011
Semi-Major Axis7,519 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1969-11-24
Launch Site
Plesetsk Cosmodrome, Russia
Int'l Designator
1969-103B
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 1969-11-24 from Plesetsk Cosmodrome, Russia on the Sfera launch. After more than 57 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 1,140 km and 1,156 km with an inclination of 74.0°. It travels at approximately 26,211 km/h (7.28 km/s), completing one full orbit every 108 minutes — that’s roughly 13.30 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 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 1,148 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 555 active payloads and 392 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0012, ONEWEB-0010, ONEWEB-0008. 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 14 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 1,140 km (perigee) and 1,156 km (apogee), with an average altitude of approximately 1,148 km. It completes one orbit every 108 minutes, travelling at approximately 26,211 km/h (16,287 mph).
SL-8 R/B (NORAD ID 4255) 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 1969-11-24 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: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks SL-8 R/B (NORAD ID 4255) 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 26,211 km/h (16,287 mph) — roughly 7.28 km/s. It completes 13.30 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 sunrises and sunsets every 24 hours.