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SL-16 DEB

NORAD 39862 Debris LEO 1992-093LQ
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🛰️ Orbital Parameters
Perigee
612 km
Apogee
705 km
Inclination
70.8°
Period
97.9 min
Mean Motion
14.70831020 rev/day
TLE Epoch
2026-10-10 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude659 km
Orbital Velocity27,109 km/h
Velocity7.53 km/s
Orbital Period98 minutes
Orbits / Day14.71
Eccentricity0.0066
Semi-Major Axis7,030 km
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1992-12-25
Launch Site
Baikonur Cosmodrome, Kazakhstan
Int'l Designator
1992-093LQ
Object Type
Debris
RCS Size
Small (<0.1 m²)
📖 About This Object
SL-16 DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 1992-12-25 from Baikonur Cosmodrome, Kazakhstan on the Tselina-2 launch. With over 34 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 612 km and 705 km with an inclination of 70.8°. It travels at approximately 27,109 km/h (7.53 km/s), completing one full orbit every 98 minutes — that’s roughly 14.71 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 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 659 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of SL-16 DEB’s average altitude, there are currently 856 active payloads and 1,203 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, ONEWEB-0179. With an inclination of 70.8°, SL-16 DEB passes over latitudes between 70.8°N and 70.8°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 1,550 active satellites in total, of which 20 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 612 km (perigee) and 705 km (apogee), with an average altitude of approximately 659 km. It completes one orbit every 98 minutes, travelling at approximately 27,109 km/h (16,845 mph).
SL-16 DEB (NORAD ID 39862) 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 1992-12-25 from Baikonur Cosmodrome, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks SL-16 DEB (NORAD ID 39862) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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 27,109 km/h (16,845 mph) — roughly 7.53 km/s. It completes 14.71 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 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 7.53 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.