SL-16 DEB
NORAD 27690
Debris
LEO
2001-056J
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LEO · NORAD 27690
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
1006 km
Apogee
1279 km
Inclination
100.4°
Period
108.2 min
Mean Motion
13.31098694 rev/day
TLE Epoch
2026-06-20 08:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,143 km
Orbital Velocity26,221 km/h
Velocity7.28 km/s
Orbital Period108 minutes
Orbits / Day13.31
Eccentricity0.0182
Semi-Major Axis7,514 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2001-12-10
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2001-056J
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
SL-16 DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 2001-12-10 from Baikonur, Kazakhstan on the Meteor-3M 17F45 No. 101 launch. With over 25 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 1,006 km and 1,279 km with an inclination of 100.4°. It travels at approximately 26,221 km/h (7.28 km/s), completing one full orbit every 108 minutes — that’s roughly 13.31 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 years. As orbital debris, SL-16 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-16 DEB orbits at an average altitude of 1,143 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of SL-16 DEB’s average altitude, there are currently 403 active payloads and 311 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0250, ONEWEB-0316, ONEWEB-0318. With an inclination of 100.4°, SL-16 DEB passes over latitudes between 100.4°N and 100.4°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. 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-16 DEB orbits in Low Earth Orbit (LEO) at altitudes between 1,006 km (perigee) and 1,279 km (apogee), with an average altitude of approximately 1,143 km. It completes one orbit every 108 minutes, travelling at approximately 26,221 km/h (16,293 mph).
SL-16 DEB (NORAD ID 27690) 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-16 DEB was launched on 2001-12-10 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: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks SL-16 DEB (NORAD ID 27690) 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-16 DEB travels at approximately 26,221 km/h (16,293 mph) — roughly 7.28 km/s. It completes 13.31 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 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 7.28 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-16 DEB. Read more about debris statistics and the Kessler syndrome.