SL-3 R/B
NORAD 10515
Rocket Body
LEO
1977-117B
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LEO · NORAD 10515
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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
847 km
Apogee
878 km
Inclination
81.2°
Period
102.2 min
Mean Motion
14.09108669 rev/day
TLE Epoch
2026-06-25 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude863 km
Orbital Velocity26,724 km/h
Velocity7.42 km/s
Orbital Period102 minutes
Orbits / Day14.09
Eccentricity0.0021
Semi-Major Axis7,234 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1977-12-14
Launch Site
PKMTR
Int'l Designator
1977-117B
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 1977-12-14 from PKMTR on the Meteor-2 No. 3 launch. With over 49 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 847 km and 878 km with an inclination of 81.2°. It travels at approximately 26,724 km/h (7.42 km/s), completing one full orbit every 102 minutes — that’s roughly 14.09 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 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 863 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of SL-3 R/B’s average altitude, there are currently 220 active payloads and 1,907 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0455. 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 1,287 active satellites in total, of which 51 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 847 km (perigee) and 878 km (apogee), with an average altitude of approximately 863 km. It completes one orbit every 102 minutes, travelling at approximately 26,724 km/h (16,605 mph).
SL-3 R/B (NORAD ID 10515) 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 1977-12-14 from PKMTR. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks SL-3 R/B (NORAD ID 10515) 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 26,724 km/h (16,605 mph) — roughly 7.42 km/s. It completes 14.09 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.