SL-6 R/B(2)
NORAD 7629
Rocket Body
MEO
1975-007D
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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
6407 km
Apogee
33906 km
Inclination
68.9°
Period
716.9 min
Mean Motion
2.00855949 rev/day
TLE Epoch
2026-09-16 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude20,157 km
Orbital Velocity13,955 km/h
Velocity3.88 km/s
Orbital Period11 hours 57 minutes
Orbits / Day2.01
Eccentricity0.5183
Semi-Major Axis26,528 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1975-01-30
Launch Site
Plesetsk Cosmodrome, Russia
Int'l Designator
1975-007D
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
SL-6 R/B(2) is a spent rocket body associated with Russia (CIS), launched on 1975-01-30 from Plesetsk Cosmodrome, Russia on the Oko launch. After more than 51 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 6,407 km and 33,906 km with an inclination of 68.9°. It travels at approximately 13,955 km/h (3.88 km/s), completing one full orbit every 11 hours 57 minutes — that’s roughly 2.01 orbits per day. Its orbital eccentricity of 0.5183 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like SL-6 R/B(2) 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-6 R/B(2) orbits at an average altitude of 20,157 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-6 R/B(2)’s average altitude, there are currently 105 active payloads and 10 tracked debris or rocket body fragments. With an inclination of 68.9°, SL-6 R/B(2) passes over latitudes between 68.9°N and 68.9°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 57 share a similar altitude band with SL-6 R/B(2).
🔗 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-6 R/B(2) orbits in Medium Earth Orbit (MEO) at altitudes between 6,407 km (perigee) and 33,906 km (apogee), with an average altitude of approximately 20,157 km. It completes one orbit every 11 hours 57 minutes, travelling at approximately 13,955 km/h (8,671 mph).
SL-6 R/B(2) (NORAD ID 7629) 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-6 R/B(2) was launched on 1975-01-30 from Plesetsk Cosmodrome, Russia, Russia’s northern military cosmodrome, used primarily for high-inclination and polar orbit launches. View the full satellite launch log.
Yes — Orbital Radar tracks SL-6 R/B(2) (NORAD ID 7629) 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-6 R/B(2) travels at approximately 13,955 km/h (8,671 mph) — roughly 3.88 km/s. It completes 2.01 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.