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SL-11 R/B

NORAD 4597 Rocket Body MEO 1970-089B
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
513 km
Apogee
2044 km
Inclination
62.9°
Period
111.1 min
Mean Motion
12.95712851 rev/day
TLE Epoch
2026-09-15 10:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,279 km
Orbital Velocity25,987 km/h
Velocity7.22 km/s
Orbital Period111 minutes
Orbits / Day12.96
Eccentricity0.1001
Semi-Major Axis7,650 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1970-10-23
Launch Site
Baikonur Cosmodrome, Kazakhstan
Int'l Designator
1970-089B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
SL-11 R/B is a spent rocket body associated with Russia (CIS), launched on 1970-10-23 from Baikonur Cosmodrome, Kazakhstan on the I2P launch. After more than 56 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Medium Earth Orbit (MEO) at altitudes between 513 km and 2,044 km with an inclination of 62.9°. It travels at approximately 25,987 km/h (7.22 km/s), completing one full orbit every 111 minutes — that’s roughly 12.96 orbits per day. Its orbital eccentricity of 0.1001 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. Spent rocket bodies like SL-11 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-11 R/B orbits at an average altitude of 1,279 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of SL-11 R/B’s average altitude, there are currently 20 active payloads and 381 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 62.9°, SL-11 R/B passes over latitudes between 62.9°N and 62.9°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 1,537 active satellites in total, of which 5 share a similar altitude band with SL-11 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-11 R/B orbits in Medium Earth Orbit (MEO) at altitudes between 513 km (perigee) and 2,044 km (apogee), with an average altitude of approximately 1,279 km. It completes one orbit every 111 minutes, travelling at approximately 25,987 km/h (16,148 mph).
SL-11 R/B (NORAD ID 4597) 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-11 R/B was launched on 1970-10-23 from Baikonur Cosmodrome, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. At its current altitude, the estimated remaining orbital lifetime is: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks SL-11 R/B (NORAD ID 4597) 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-11 R/B travels at approximately 25,987 km/h (16,148 mph) — roughly 7.22 km/s. It completes 12.96 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 26 sunrises and sunsets every 24 hours.