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SL-12 DEB

NORAD 23616 Debris MEO 1992-047J
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
250 km
Apogee
6414 km
Inclination
64.2°
Period
158.7 min
Mean Motion
9.07366964 rev/day
TLE Epoch
2026-06-20 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude3,332 km
Orbital Velocity23,074 km/h
Velocity6.41 km/s
Orbital Period2 hours 39 minutes
Orbits / Day9.07
Eccentricity0.3176
Semi-Major Axis9,703 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1992-07-30
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1992-047J
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 1992-07-30 from Baikonur, Kazakhstan on the Uragan No. 56L launch. With over 34 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 250 km and 6,414 km with an inclination of 64.2°. It travels at approximately 23,074 km/h (6.41 km/s), completing one full orbit every 2 hours 39 minutes — that’s roughly 9.07 orbits per day. Its orbital eccentricity of 0.3176 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 3,332 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 1 active payload and 1 tracked debris or rocket body fragment. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 64.2°, SL-12 DEB passes over latitudes between 64.2°N and 64.2°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 250 km (perigee) and 6,414 km (apogee), with an average altitude of approximately 3,332 km. It completes one orbit every 2 hours 39 minutes, travelling at approximately 23,074 km/h (14,337 mph).
SL-12 DEB (NORAD ID 23616) 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 1992-07-30 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 23616) 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 23,074 km/h (14,337 mph) — roughly 6.41 km/s. It completes 9.07 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 18 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 6.41 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.