SL-3 R/B
NORAD 5118
Rocket Body
LEO
1971-028B
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
326 km
Apogee
337 km
Inclination
81.2°
Period
91.2 min
Mean Motion
15.79921943 rev/day
TLE Epoch
2026-09-16 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude332 km
Orbital Velocity27,762 km/h
Velocity7.71 km/s
Orbital Period91 minutes
Orbits / Day15.80
Eccentricity0.0008
Semi-Major Axis6,703 km
Est. Orbital LifetimeMonths to ~1 year
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1971-04-07
Launch Site
Plesetsk Cosmodrome, Russia
Int'l Designator
1971-028B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
SL-3 R/B is a spent rocket body associated with Russia (CIS), launched on 1971-04-07 from Plesetsk Cosmodrome, Russia on the Tselina-D launch. After more than 55 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 326 km and 337 km with an inclination of 81.2°. It travels at approximately 27,762 km/h (7.71 km/s), completing one full orbit every 91 minutes — that’s roughly 15.80 orbits per day. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is months to ~1 year. Spent rocket bodies like SL-3 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-3 R/B orbits at an average altitude of 332 km in the lower reaches of Low Earth Orbit, where atmospheric drag is significant and orbital lifetimes are measured in months to a few years. This is the busiest corridor in space — home to crewed spacecraft, rapid-revisit imaging satellites and the densest part of the Starlink constellation. Within ±50 km of SL-3 R/B’s average altitude, there are currently 1,143 active payloads and 38 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1020. This makes it one of the more crowded altitude bands, containing roughly 6.1% of all active satellites. With an inclination of 81.2°, SL-3 R/B passes over latitudes between 81.2°N and 81.2°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 23 share a similar altitude band with SL-3 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-3 R/B orbits in Low Earth Orbit (LEO) at altitudes between 326 km (perigee) and 337 km (apogee), with an average altitude of approximately 332 km. It completes one orbit every 91 minutes, travelling at approximately 27,762 km/h (17,251 mph).
SL-3 R/B (NORAD ID 5118) 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-3 R/B was launched on 1971-04-07 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: months to ~1 year. View the full satellite launch log.
Yes — Orbital Radar tracks SL-3 R/B (NORAD ID 5118) 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-3 R/B travels at approximately 27,762 km/h (17,251 mph) — roughly 7.71 km/s. It completes 15.80 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 32 sunrises and sunsets every 24 hours.