SL-12 DEB
NORAD 23294
Debris
MEO
1985-118R
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MEO · NORAD 23294
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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
446 km
Apogee
16769 km
Inclination
65.1°
Period
304.3 min
Mean Motion
4.73250784 rev/day
TLE Epoch
2026-06-13 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude8,608 km
Orbital Velocity18,571 km/h
Velocity5.16 km/s
Orbital Period5 hours 4 minutes
Orbits / Day4.73
Eccentricity0.5449
Semi-Major Axis14,979 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1985-12-24
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1985-118R
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
SL-12 DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 1985-12-24 from Baikonur, Kazakhstan on the Uragan No. 22L launch. With over 41 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 446 km and 16,769 km with an inclination of 65.1°. It travels at approximately 18,571 km/h (5.16 km/s), completing one full orbit every 5 hours 4 minutes — that’s roughly 4.73 orbits per day. Its orbital eccentricity of 0.5449 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. As orbital debris, SL-12 DEB poses a potential collision risk to operational satellites in nearby orbits and is continuously monitored by the U.S. Space Surveillance Network and other tracking systems.
🌍 Orbit Context
SL-12 DEB orbits at an average altitude of 8,608 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-12 DEB’s average altitude, there are currently 0 active payloads and 9 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 65.1°, SL-12 DEB 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 1,285 active satellites in total.
🔗 Tracked Space Debris
This is a tracked piece of orbital debris — a fragment from a collision, explosion, or separation event that no longer serves any useful purpose. Space surveillance networks catalogue objects larger than approximately 10 cm in LEO. Even small debris can be catastrophic at orbital velocities (7–8 km/s in LEO), carrying kinetic energy comparable to a hand grenade per centimetre-sized fragment. The growing debris population is one of the most pressing challenges for long-term space sustainability.
❓ Frequently Asked Questions
SL-12 DEB orbits in Medium Earth Orbit (MEO) at altitudes between 446 km (perigee) and 16,769 km (apogee), with an average altitude of approximately 8,608 km. It completes one orbit every 5 hours 4 minutes, travelling at approximately 18,571 km/h (11,540 mph).
SL-12 DEB (NORAD ID 23294) is a piece of tracked orbital debris attributed to Russia (CIS). It was likely created by a fragmentation event, collision, or mission-related separation. Even small debris objects at orbital velocities carry enormous kinetic energy, so they are tracked by the U.S. Space Surveillance Network to enable collision avoidance for operational satellites.
SL-12 DEB was launched on 1985-12-24 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-12 DEB (NORAD ID 23294) 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-12 DEB travels at approximately 18,571 km/h (11,540 mph) — roughly 5.16 km/s. It completes 4.73 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 9 sunrises and sunsets every 24 hours.
All tracked debris poses a potential collision risk to operational satellites. At orbital velocities, even a small object carries enormous kinetic energy — a 1 cm fragment at 5.16 km/s has the energy equivalent of a hand grenade. Space agencies perform routine conjunction assessments and may manoeuvre operational satellites to avoid tracked objects like SL-12 DEB. Read more about debris statistics and the Kessler syndrome.