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SL-3 R/B

NORAD 13819 Rocket Body LEO 1983-010B
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🛰️ Orbital Parameters
Perigee
401 km
Apogee
420 km
Inclination
81.1°
Period
92.8 min
Mean Motion
15.52082782 rev/day
TLE Epoch
2026-10-14 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude411 km
Orbital Velocity27,600 km/h
Velocity7.67 km/s
Orbital Period93 minutes
Orbits / Day15.52
Eccentricity0.0014
Semi-Major Axis6,782 km
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1983-02-16
Launch Site
Plesetsk Cosmodrome, Russia
Int'l Designator
1983-010B
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 1983-02-16 from Plesetsk Cosmodrome, Russia on the Tselina-D launch. With over 43 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 401 km and 420 km with an inclination of 81.1°. It travels at approximately 27,600 km/h (7.67 km/s), completing one full orbit every 93 minutes — that’s roughly 15.52 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~1–3 years. 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 411 km in the core of Low Earth Orbit, the most heavily utilised altitude band. The balance of moderate drag (limiting debris accumulation) and short signal path (enabling low-latency links and high-resolution imaging) makes this regime the default for most commercial and government missions. Within ±50 km of SL-3 R/B’s average altitude, there are currently 847 active payloads and 99 tracked debris or rocket body fragments — notable neighbours include ISS (ZARYA), STARLINK-1008, STARLINK-1012. With an inclination of 81.1°, SL-3 R/B passes over latitudes between 81.1°N and 81.1°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 1,514 active satellites in total, of which 32 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 401 km (perigee) and 420 km (apogee), with an average altitude of approximately 411 km. It completes one orbit every 93 minutes, travelling at approximately 27,600 km/h (17,150 mph).
SL-3 R/B (NORAD ID 13819) 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 1983-02-16 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: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks SL-3 R/B (NORAD ID 13819) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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 27,600 km/h (17,150 mph) — roughly 7.67 km/s. It completes 15.52 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.