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SL-3 R/B

NORAD 10114 Rocket Body LEO 1977-057B
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
419 km
Apogee
426 km
Inclination
97.6°
Period
93.0 min
Mean Motion
15.48047220 rev/day
TLE Epoch
2026-06-25 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude423 km
Orbital Velocity27,576 km/h
Velocity7.66 km/s
Orbital Period93 minutes
Orbits / Day15.48
Eccentricity0.0005
Semi-Major Axis6,794 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1977-06-29
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1977-057B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
SL-3 R/B is a spent rocket body associated with Russia (CIS), launched on 1977-06-29 from Baikonur, Kazakhstan on the Meteor-Priroda No. 2-2 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 419 km and 426 km with an inclination of 97.6°. It travels at approximately 27,576 km/h (7.66 km/s), completing one full orbit every 93 minutes — that’s roughly 15.48 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~1–3 years. Spent rocket bodies like SL-3 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-3 R/B orbits at an average altitude of 423 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of SL-3 R/B’s average altitude, there are currently 3,498 active payloads and 133 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1017. This makes it one of the more crowded altitude bands, containing roughly 20% of all active satellites. With an inclination of 97.6°, SL-3 R/B passes over latitudes between 97.6°N and 97.6°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 43 share a similar altitude band with SL-3 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-3 R/B is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 423 km altitude. Its 97.6° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 93 minutes, travelling at 27,576 km/h.
SL-3 R/B (NORAD ID 10114) 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-3 R/B was launched on 1977-06-29 from Baikonur, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks SL-3 R/B (NORAD ID 10114) 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-3 R/B travels at approximately 27,576 km/h (17,135 mph) — roughly 7.66 km/s. It completes 15.48 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.