SL-6 DEB
NORAD 13904
Debris
MEO
1981-088G
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MEO · NORAD 13904
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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
726 km
Apogee
13685 km
Inclination
63.0°
Period
262.6 min
Mean Motion
5.48376982 rev/day
TLE Epoch
2026-06-19 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude7,206 km
Orbital Velocity19,506 km/h
Velocity5.42 km/s
Orbital Period4 hours 23 minutes
Orbits / Day5.48
Eccentricity0.4773
Semi-Major Axis13,577 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1981-09-11
Launch Site
PKMTR
Int'l Designator
1981-088G
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
SL-6 DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 1981-09-11 from PKMTR on the Molniya-3 No. 28 launch. With over 45 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 726 km and 13,685 km with an inclination of 63.0°. It travels at approximately 19,506 km/h (5.42 km/s), completing one full orbit every 4 hours 23 minutes — that’s roughly 5.48 orbits per day. Its orbital eccentricity of 0.4773 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. As orbital debris, SL-6 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-6 DEB orbits at an average altitude of 7,206 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-6 DEB’s average altitude, there are currently 2 active payloads and 5 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 63.0°, SL-6 DEB passes over latitudes between 63.0°N and 63.0°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-6 DEB orbits in Medium Earth Orbit (MEO) at altitudes between 726 km (perigee) and 13,685 km (apogee), with an average altitude of approximately 7,206 km. It completes one orbit every 4 hours 23 minutes, travelling at approximately 19,506 km/h (12,121 mph).
SL-6 DEB (NORAD ID 13904) 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-6 DEB was launched on 1981-09-11 from PKMTR. 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-6 DEB (NORAD ID 13904) 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-6 DEB travels at approximately 19,506 km/h (12,121 mph) — roughly 5.42 km/s. It completes 5.48 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 5.42 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-6 DEB. Read more about debris statistics and the Kessler syndrome.