SL-16 DEB
NORAD 20629
Debris
LEO
1990-046F
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LEO · NORAD 20629
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
840 km
Apogee
1129 km
Inclination
71.0°
Period
104.8 min
Mean Motion
13.74162741 rev/day
TLE Epoch
2026-06-15 11:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude985 km
Orbital Velocity26,501 km/h
Velocity7.36 km/s
Orbital Period105 minutes
Orbits / Day13.74
Eccentricity0.0196
Semi-Major Axis7,356 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1990-05-22
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1990-046F
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 1990-05-22 from Baikonur, Kazakhstan. With over 36 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 840 km and 1,129 km with an inclination of 71.0°. It travels at approximately 26,501 km/h (7.36 km/s), completing one full orbit every 105 minutes — that’s roughly 13.74 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 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 985 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 282 active payloads and 919 tracked debris or rocket body fragments. With an inclination of 71.0°, SL-16 DEB passes over latitudes between 71.0°N and 71.0°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 1,286 active satellites in total, of which 158 share a similar altitude band with SL-16 DEB.
🔗 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 840 km (perigee) and 1,129 km (apogee), with an average altitude of approximately 985 km. It completes one orbit every 105 minutes, travelling at approximately 26,501 km/h (16,467 mph).
SL-16 DEB (NORAD ID 20629) 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 1990-05-22 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: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks SL-16 DEB (NORAD ID 20629) 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 26,501 km/h (16,467 mph) — roughly 7.36 km/s. It completes 13.74 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 7.36 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.