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SL-8 R/B

NORAD 1589 Rocket Body LEO 1965-073F
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
1410 km
Apogee
1663 km
Inclination
56.0°
Period
116.8 min
Mean Motion
12.33054710 rev/day
TLE Epoch
2026-09-16 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,537 km
Orbital Velocity25,559 km/h
Velocity7.10 km/s
Orbital Period117 minutes
Orbits / Day12.33
Eccentricity0.0160
Semi-Major Axis7,908 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1965-09-18
Launch Site
Baikonur Cosmodrome, Kazakhstan
Int'l Designator
1965-073F
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 1965-09-18 from Baikonur Cosmodrome, Kazakhstan on the Strela-1 launch. After more than 61 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 1,410 km and 1,663 km with an inclination of 56.0°. It travels at approximately 25,559 km/h (7.10 km/s), completing one full orbit every 117 minutes — that’s roughly 12.33 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 1,537 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 167 active payloads and 399 tracked debris or rocket body fragments. With an inclination of 56.0°, SL-8 R/B passes over latitudes between 56.0°N and 56.0°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 148 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 1,410 km (perigee) and 1,663 km (apogee), with an average altitude of approximately 1,537 km. It completes one orbit every 117 minutes, travelling at approximately 25,559 km/h (15,882 mph).
SL-8 R/B (NORAD ID 1589) 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 1965-09-18 from Baikonur Cosmodrome, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. 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 1589) 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 25,559 km/h (15,882 mph) — roughly 7.10 km/s. It completes 12.33 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 25 sunrises and sunsets every 24 hours.