SL-8 R/B
NORAD 9013
Rocket Body
MEO
1976-067B
CONNECTING…
MEO · NORAD 9013
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
960 km
Apogee
2092 km
Inclination
65.9°
Period
116.6 min
Mean Motion
12.35417769 rev/day
TLE Epoch
2026-09-16 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,526 km
Orbital Velocity25,576 km/h
Velocity7.10 km/s
Orbital Period117 minutes
Orbits / Day12.35
Eccentricity0.0717
Semi-Major Axis7,897 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1976-07-08
Launch Site
Plesetsk Cosmodrome, Russia
Int'l Designator
1976-067B
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 1976-07-08 from Plesetsk Cosmodrome, Russia on the Lira launch. After more than 50 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Medium Earth Orbit (MEO) at altitudes between 960 km and 2,092 km with an inclination of 65.9°. It travels at approximately 25,576 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 1,526 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of SL-8 R/B’s average altitude, there are currently 211 active payloads and 392 tracked debris or rocket body fragments. With an inclination of 65.9°, SL-8 R/B passes over latitudes between 65.9°N and 65.9°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 197 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 Medium Earth Orbit (MEO) at altitudes between 960 km (perigee) and 2,092 km (apogee), with an average altitude of approximately 1,526 km. It completes one orbit every 117 minutes, travelling at approximately 25,576 km/h (15,892 mph).
SL-8 R/B (NORAD ID 9013) 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 1976-07-08 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 9013) 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 25,576 km/h (15,892 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.