SL-14 R/B
NORAD 10096
Rocket Body
LEO
1977-055B
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LEO · NORAD 10096
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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
563 km
Apogee
619 km
Inclination
75.8°
Period
96.5 min
Mean Motion
14.92144771 rev/day
TLE Epoch
2026-06-26 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude591 km
Orbital Velocity27,240 km/h
Velocity7.57 km/s
Orbital Period97 minutes
Orbits / Day14.92
Eccentricity0.0040
Semi-Major Axis6,962 km
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1977-06-24
Launch Site
PKMTR
Int'l Designator
1977-055B
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 1977-06-24 from PKMTR on the EPN No. 03.0380 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 563 km and 619 km with an inclination of 75.8°. It travels at approximately 27,240 km/h (7.57 km/s), completing one full orbit every 97 minutes — that’s roughly 14.92 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 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 591 km in the core of Low Earth Orbit, the most heavily utilised altitude band. The balance of moderate drag (limiting debris accumulation) and short signal path (enabling low-latency links and high-resolution imaging) makes this regime the default for most commercial and government missions. Within ±50 km of SL-14 R/B’s average altitude, there are currently 2,129 active payloads and 609 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3005, STARLINK-3090. This makes it one of the more crowded altitude bands, containing roughly 12.2% of all active satellites. With an inclination of 75.8°, SL-14 R/B passes over latitudes between 75.8°N and 75.8°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. Russia (CIS) operates approximately 1,286 active satellites in total, of which 31 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 563 km (perigee) and 619 km (apogee), with an average altitude of approximately 591 km. It completes one orbit every 97 minutes, travelling at approximately 27,240 km/h (16,926 mph).
SL-14 R/B (NORAD ID 10096) 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 1977-06-24 from PKMTR. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks SL-14 R/B (NORAD ID 10096) 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 27,240 km/h (16,926 mph) — roughly 7.57 km/s. It completes 14.92 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.