SL-8 R/B
NORAD 7095
Rocket Body
LEO
1974-001B
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🛰️ Orbital Parameters
Perigee
940 km
Apogee
995 km
Inclination
83.0°
Period
104.4 min
Mean Motion
13.79071630 rev/day
TLE Epoch
2026-09-16 02:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude968 km
Orbital Velocity26,532 km/h
Velocity7.37 km/s
Orbital Period104 minutes
Orbits / Day13.79
Eccentricity0.0037
Semi-Major Axis7,339 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1974-01-17
Launch Site
Plesetsk Cosmodrome, Russia
Int'l Designator
1974-001B
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 1974-01-17 from Plesetsk Cosmodrome, Russia on the Zaliv launch. After more than 52 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 940 km and 995 km with an inclination of 83.0°. It travels at approximately 26,532 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 968 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 374 active payloads and 1,209 tracked debris or rocket body fragments. With an inclination of 83.0°, SL-8 R/B passes over latitudes between 83.0°N and 83.0°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. Russia (CIS) operates approximately 1,537 active satellites in total, of which 204 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 940 km (perigee) and 995 km (apogee), with an average altitude of approximately 968 km. It completes one orbit every 104 minutes, travelling at approximately 26,532 km/h (16,486 mph).
SL-8 R/B (NORAD ID 7095) 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 1974-01-17 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 7095) 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 26,532 km/h (16,486 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.