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SL-8 R/B

NORAD 10962 Rocket Body LEO 1978-063B
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
731 km
Apogee
766 km
Inclination
74.1°
Period
99.8 min
Mean Motion
14.42903339 rev/day
TLE Epoch
2026-06-25 16:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude749 km
Orbital Velocity26,937 km/h
Velocity7.48 km/s
Orbital Period100 minutes
Orbits / Day14.43
Eccentricity0.0025
Semi-Major Axis7,120 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1978-06-21
Launch Site
PKMTR
Int'l Designator
1978-063B
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 1978-06-21 from PKMTR on the Strela-2M launch. With over 48 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 731 km and 766 km with an inclination of 74.1°. It travels at approximately 26,937 km/h (7.48 km/s), completing one full orbit every 100 minutes — that’s roughly 14.43 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 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 749 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of SL-8 R/B’s average altitude, there are currently 356 active payloads and 1,955 tracked debris or rocket body fragments — notable neighbours include LANDSAT 9. 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 1,287 active satellites in total, of which 47 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 731 km (perigee) and 766 km (apogee), with an average altitude of approximately 749 km. It completes one orbit every 100 minutes, travelling at approximately 26,937 km/h (16,738 mph).
SL-8 R/B (NORAD ID 10962) 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 1978-06-21 from PKMTR. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks SL-8 R/B (NORAD ID 10962) 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 26,937 km/h (16,738 mph) — roughly 7.48 km/s. It completes 14.43 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.