SL-3 R/B
NORAD 877
Rocket Body
LEO
1964-053B
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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
634 km
Apogee
743 km
Inclination
65.1°
Period
98.5 min
Mean Motion
14.61463556 rev/day
TLE Epoch
2026-09-16 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude689 km
Orbital Velocity27,051 km/h
Velocity7.51 km/s
Orbital Period99 minutes
Orbits / Day14.61
Eccentricity0.0077
Semi-Major Axis7,060 km
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1964-08-28
Launch Site
Baikonur Cosmodrome, Kazakhstan
Int'l Designator
1964-053B
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 1964-08-28 from Baikonur Cosmodrome, Kazakhstan on the Meteor 11F614 No. 1 launch. After more than 62 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Low Earth Orbit (LEO) at altitudes between 634 km and 743 km with an inclination of 65.1°. It travels at approximately 27,051 km/h (7.51 km/s), completing one full orbit every 99 minutes — that’s roughly 14.61 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 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 689 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-3 R/B’s average altitude, there are currently 339 active payloads and 1,435 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, ONEWEB-0179. With an inclination of 65.1°, SL-3 R/B passes over latitudes between 65.1°N and 65.1°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 20 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 orbits in Low Earth Orbit (LEO) at altitudes between 634 km (perigee) and 743 km (apogee), with an average altitude of approximately 689 km. It completes one orbit every 99 minutes, travelling at approximately 27,051 km/h (16,809 mph).
SL-3 R/B (NORAD ID 877) 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 1964-08-28 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: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks SL-3 R/B (NORAD ID 877) 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 27,051 km/h (16,809 mph) — roughly 7.51 km/s. It completes 14.61 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.