SL-4 R/B
NORAD 100713
Rocket Body
LEO
2026-212B
CONNECTING…
LEO · NORAD 100713
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
171 km
Apogee
194 km
Inclination
51.7°
Period
88.1 min
Mean Motion
16.33714955 rev/day
TLE Epoch
2026-09-18 13:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude183 km
Orbital Velocity28,076 km/h
Velocity7.80 km/s
Orbital Period88 minutes
Orbits / Day16.34
Eccentricity0.0018
Semi-Major Axis6,554 km
Est. Orbital LifetimeDays to weeks — very low orbit, rapid decay
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2026-09-16
Launch Site
Baikonur Cosmodrome, Kazakhstan
Int'l Designator
2026-212B
Object Type
Rocket Body
RCS Size
Unknown
📖 About This Object
SL-4 R/B is a spent rocket body associated with Russia (CIS), launched on 2026-09-16 from Baikonur Cosmodrome, Kazakhstan on the Progress 7K-TGM No. 465 launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 171 km and 194 km with an inclination of 51.7°. It travels at approximately 28,076 km/h (7.80 km/s), completing one full orbit every 88 minutes — that’s roughly 16.34 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is days to weeks — very low orbit, rapid decay. Spent rocket bodies like SL-4 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-4 R/B orbits at an average altitude of 183 km in the lower reaches of Low Earth Orbit, where atmospheric drag is significant and orbital lifetimes are measured in months to a few years. This is the busiest corridor in space — home to crewed spacecraft, rapid-revisit imaging satellites and the densest part of the Starlink constellation. Within ±50 km of SL-4 R/B’s average altitude, there are currently 17 active payloads and 2 tracked debris or rocket body fragments — notable neighbours include STARLINK-1319, STARLINK-1724, STARLINK-1942. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 51.7°, SL-4 R/B passes over latitudes between 51.7°N and 51.7°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 1,536 active satellites in total.
🔗 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-4 R/B orbits in Low Earth Orbit (LEO) at altitudes between 171 km (perigee) and 194 km (apogee), with an average altitude of approximately 183 km. It completes one orbit every 88 minutes, travelling at approximately 28,076 km/h (17,446 mph).
SL-4 R/B (NORAD ID 100713) 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-4 R/B was launched on 2026-09-16 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: days to weeks — very low orbit, rapid decay. View the full satellite launch log.
Yes — Orbital Radar tracks SL-4 R/B (NORAD ID 100713) 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-4 R/B travels at approximately 28,076 km/h (17,446 mph) — roughly 7.80 km/s. It completes 16.34 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 33 sunrises and sunsets every 24 hours.