Skip to content
Home Library Satellite Directory SL-12 DEB

SL-12 DEB

NORAD 29323 Debris MEO 1989-039AE
CONNECTING… MEO · NORAD 29323
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
434 km
Apogee
14498 km
Inclination
64.8°
Period
270.2 min
Mean Motion
5.32977606 rev/day
TLE Epoch
2026-06-18 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude7,466 km
Orbital Velocity19,322 km/h
Velocity5.37 km/s
Orbital Period4 hours 30 minutes
Orbits / Day5.33
Eccentricity0.5082
Semi-Major Axis13,837 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1989-05-31
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1989-039AE
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 1989-05-31 from Baikonur, Kazakhstan on the Uragan No. 28L launch. With over 37 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 434 km and 14,498 km with an inclination of 64.8°. It travels at approximately 19,322 km/h (5.37 km/s), completing one full orbit every 4 hours 30 minutes — that’s roughly 5.33 orbits per day. Its orbital eccentricity of 0.5082 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 7,466 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 3 active payloads and 12 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-12 DEB 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 1,285 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 434 km (perigee) and 14,498 km (apogee), with an average altitude of approximately 7,466 km. It completes one orbit every 4 hours 30 minutes, travelling at approximately 19,322 km/h (12,006 mph).
SL-12 DEB (NORAD ID 29323) 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 1989-05-31 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 29323) 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 19,322 km/h (12,006 mph) — roughly 5.37 km/s. It completes 5.33 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 11 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 5.37 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.