SL-14 R/B
NORAD 11087
Rocket Body
LEO
1978-100D
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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
1686 km
Apogee
1703 km
Inclination
82.5°
Period
120.3 min
Mean Motion
11.97035551 rev/day
TLE Epoch
2026-10-15 02:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,695 km
Orbital Velocity25,308 km/h
Velocity7.03 km/s
Orbital Period2 hours
Orbits / Day11.97
Eccentricity0.0011
Semi-Major Axis8,066 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1978-10-26
Launch Site
Plesetsk Cosmodrome, Russia
Int'l Designator
1978-100D
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
SL-14 R/B is a spent rocket body associated with Russia (CIS), launched on 1978-10-26 from Plesetsk Cosmodrome, Russia on the Meteor-2 GVM 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 1,686 km and 1,703 km with an inclination of 82.5°. It travels at approximately 25,308 km/h (7.03 km/s), completing one full orbit every 2 hours — that’s roughly 11.97 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. Spent rocket bodies like SL-14 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-14 R/B orbits at an average altitude of 1,695 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-14 R/B’s average altitude, there are currently 21 active payloads and 77 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 82.5°, SL-14 R/B passes over latitudes between 82.5°N and 82.5°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 7 share a similar altitude band with SL-14 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-14 R/B orbits in Low Earth Orbit (LEO) at altitudes between 1,686 km (perigee) and 1,703 km (apogee), with an average altitude of approximately 1,695 km. It completes one orbit every 2 hours, travelling at approximately 25,308 km/h (15,726 mph).
SL-14 R/B (NORAD ID 11087) 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-14 R/B was launched on 1978-10-26 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: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks SL-14 R/B (NORAD ID 11087) 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-14 R/B travels at approximately 25,308 km/h (15,726 mph) — roughly 7.03 km/s. It completes 11.97 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 24 sunrises and sunsets every 24 hours.