SL-19 R/B
NORAD 23440
Rocket Body
MEO
1994-085B
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
1872 km
Apogee
2177 km
Inclination
64.8°
Period
127.8 min
Mean Motion
11.27134202 rev/day
TLE Epoch
2026-06-25 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude2,025 km
Orbital Velocity24,806 km/h
Velocity6.89 km/s
Orbital Period2 hours 8 minutes
Orbits / Day11.27
Eccentricity0.0182
Semi-Major Axis8,396 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1994-12-26
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1994-085B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
SL-19 R/B is a spent rocket body associated with Russia (CIS), launched on 1994-12-26 from Baikonur, Kazakhstan on the Radio-ROSTO launch. With over 32 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 1,872 km and 2,177 km with an inclination of 64.8°. It travels at approximately 24,806 km/h (6.89 km/s), completing one full orbit every 2 hours 8 minutes — that’s roughly 11.27 orbits per day. Spent rocket bodies like SL-19 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-19 R/B orbits at an average altitude of 2,025 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-19 R/B’s average altitude, there are currently 8 active payloads and 28 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 64.8°, SL-19 R/B passes over latitudes between 64.8°N and 64.8°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 1,286 active satellites in total, of which 2 share a similar altitude band with SL-19 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-19 R/B orbits in Medium Earth Orbit (MEO) at altitudes between 1,872 km (perigee) and 2,177 km (apogee), with an average altitude of approximately 2,025 km. It completes one orbit every 2 hours 8 minutes, travelling at approximately 24,806 km/h (15,413 mph).
SL-19 R/B (NORAD ID 23440) 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-19 R/B was launched on 1994-12-26 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: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks SL-19 R/B (NORAD ID 23440) 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-19 R/B travels at approximately 24,806 km/h (15,413 mph) — roughly 6.89 km/s. It completes 11.27 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 23 sunrises and sunsets every 24 hours.