Skip to content
Home Library Satellite Directory SL-8 R/B

SL-8 R/B

NORAD 7426 Rocket Body LEO 1974-069B
CONNECTING… LEO · NORAD 7426
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
1353 km
Apogee
1420 km
Inclination
74.1°
Period
113.5 min
Mean Motion
12.68867008 rev/day
TLE Epoch
2026-09-16 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,387 km
Orbital Velocity25,805 km/h
Velocity7.17 km/s
Orbital Period113 minutes
Orbits / Day12.69
Eccentricity0.0043
Semi-Major Axis7,758 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1974-08-29
Launch Site
Plesetsk Cosmodrome, Russia
Int'l Designator
1974-069B
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 1974-08-29 from Plesetsk Cosmodrome, Russia on the Geoid 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 1,353 km and 1,420 km with an inclination of 74.1°. It travels at approximately 25,805 km/h (7.17 km/s), completing one full orbit every 113 minutes — that’s roughly 12.69 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 1,387 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 253 active payloads and 243 tracked debris or rocket body fragments. With an inclination of 74.1°, SL-8 R/B passes over latitudes between 74.1°N and 74.1°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 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 1,353 km (perigee) and 1,420 km (apogee), with an average altitude of approximately 1,387 km. It completes one orbit every 113 minutes, travelling at approximately 25,805 km/h (16,035 mph).
SL-8 R/B (NORAD ID 7426) 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 1974-08-29 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 7426) 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 25,805 km/h (16,035 mph) — roughly 7.17 km/s. It completes 12.69 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 25 sunrises and sunsets every 24 hours.