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SL-14 R/B

NORAD 23659 Rocket Body LEO 1995-046C
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
612 km
Apogee
644 km
Inclination
82.5°
Period
97.3 min
Mean Motion
14.80389974 rev/day
TLE Epoch
2026-06-26 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude628 km
Orbital Velocity27,168 km/h
Velocity7.55 km/s
Orbital Period97 minutes
Orbits / Day14.80
Eccentricity0.0023
Semi-Major Axis6,999 km
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1995-08-31
Launch Site
PKMTR
Int'l Designator
1995-046C
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 1995-08-31 from PKMTR on the Okean-O1 No. 8/NKhM 10 launch. With over 31 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 612 km and 644 km with an inclination of 82.5°. It travels at approximately 27,168 km/h (7.55 km/s), completing one full orbit every 97 minutes — that’s roughly 14.80 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 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 628 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of SL-14 R/B’s average altitude, there are currently 799 active payloads and 828 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-5823, STARLINK-34374. 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 16 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 612 km (perigee) and 644 km (apogee), with an average altitude of approximately 628 km. It completes one orbit every 97 minutes, travelling at approximately 27,168 km/h (16,881 mph).
SL-14 R/B (NORAD ID 23659) 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 1995-08-31 from PKMTR. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks SL-14 R/B (NORAD ID 23659) 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 27,168 km/h (16,881 mph) — roughly 7.55 km/s. It completes 14.80 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.