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SL-14 R/B

NORAD 21233 Rocket Body LEO 1991-030B
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
1185 km
Apogee
1212 km
Inclination
82.5°
Period
109.4 min
Mean Motion
13.16389258 rev/day
TLE Epoch
2026-06-26 02:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,199 km
Orbital Velocity26,124 km/h
Velocity7.26 km/s
Orbital Period109 minutes
Orbits / Day13.16
Eccentricity0.0018
Semi-Major Axis7,570 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1991-04-24
Launch Site
PKMTR
Int'l Designator
1991-030B
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 1991-04-24 from PKMTR on the Meteor-3 No. 6 launch. With over 35 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 1,185 km and 1,212 km with an inclination of 82.5°. It travels at approximately 26,124 km/h (7.26 km/s), completing one full orbit every 109 minutes — that’s roughly 13.16 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 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 1,199 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-14 R/B’s average altitude, there are currently 843 active payloads and 210 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0012, ONEWEB-0010, ONEWEB-0008. 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 1,286 active satellites in total, of which 8 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 1,185 km (perigee) and 1,212 km (apogee), with an average altitude of approximately 1,199 km. It completes one orbit every 109 minutes, travelling at approximately 26,124 km/h (16,233 mph).
SL-14 R/B (NORAD ID 21233) 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 1991-04-24 from PKMTR. At its current altitude, the estimated remaining orbital lifetime is: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks SL-14 R/B (NORAD ID 21233) 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 26,124 km/h (16,233 mph) — roughly 7.26 km/s. It completes 13.16 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 26 sunrises and sunsets every 24 hours.