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SL-14 R/B

NORAD 16194 Rocket Body LEO 1985-100B
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
1222 km
Apogee
1249 km
Inclination
82.6°
Period
110.2 min
Mean Motion
13.06879283 rev/day
TLE Epoch
2026-06-25 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,236 km
Orbital Velocity26,060 km/h
Velocity7.24 km/s
Orbital Period110 minutes
Orbits / Day13.07
Eccentricity0.0018
Semi-Major Axis7,607 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1985-10-24
Launch Site
PKMTR
Int'l Designator
1985-100B
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 1985-10-24 from PKMTR on the Meteor-3 No. 2 launch. With over 41 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 1,222 km and 1,249 km with an inclination of 82.6°. It travels at approximately 26,060 km/h (7.24 km/s), completing one full orbit every 110 minutes — that’s roughly 13.07 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 1,236 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 523 active payloads and 304 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0012, ONEWEB-0010, ONEWEB-0008. With an inclination of 82.6°, SL-14 R/B passes over latitudes between 82.6°N and 82.6°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 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 1,222 km (perigee) and 1,249 km (apogee), with an average altitude of approximately 1,236 km. It completes one orbit every 110 minutes, travelling at approximately 26,060 km/h (16,193 mph).
SL-14 R/B (NORAD ID 16194) 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 1985-10-24 from PKMTR. 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 16194) 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-14 R/B travels at approximately 26,060 km/h (16,193 mph) — roughly 7.24 km/s. It completes 13.07 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 26 sunrises and sunsets every 24 hours.