SL-8 R/B
NORAD 6020
Rocket Body
LEO
1972-035B
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Altitude (km)
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Longitude
🛰️ Orbital Parameters
Perigee
951 km
Apogee
982 km
Inclination
74.0°
Period
104.4 min
Mean Motion
13.79167060 rev/day
TLE Epoch
2026-09-16 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude967 km
Orbital Velocity26,534 km/h
Velocity7.37 km/s
Orbital Period104 minutes
Orbits / Day13.79
Eccentricity0.0021
Semi-Major Axis7,338 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1972-05-06
Launch Site
Plesetsk Cosmodrome, Russia
Int'l Designator
1972-035B
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 1972-05-06 from Plesetsk Cosmodrome, Russia on the Tsiklon launch. After more than 54 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 951 km and 982 km with an inclination of 74.0°. It travels at approximately 26,534 km/h (7.37 km/s), completing one full orbit every 104 minutes — that’s roughly 13.79 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 967 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 375 active payloads and 1,217 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 205 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 951 km (perigee) and 982 km (apogee), with an average altitude of approximately 967 km. It completes one orbit every 104 minutes, travelling at approximately 26,534 km/h (16,487 mph).
SL-8 R/B (NORAD ID 6020) 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 1972-05-06 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 6020) 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 26,534 km/h (16,487 mph) — roughly 7.37 km/s. It completes 13.79 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.