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SL-8 DEB

NORAD 21175 Debris LEO 1991-009AN
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
1439 km
Apogee
1671 km
Inclination
73.9°
Period
117.2 min
Mean Motion
12.28585166 rev/day
TLE Epoch
2026-06-16 11:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,555 km
Orbital Velocity25,530 km/h
Velocity7.09 km/s
Orbital Period117 minutes
Orbits / Day12.29
Eccentricity0.0146
Semi-Major Axis7,926 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1991-02-12
Launch Site
PKMTR
Int'l Designator
1991-009AN
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
SL-8 DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 1991-02-12 from PKMTR. With over 35 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 1,439 km and 1,671 km with an inclination of 73.9°. It travels at approximately 25,530 km/h (7.09 km/s), completing one full orbit every 117 minutes — that’s roughly 12.29 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. As orbital debris, SL-8 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-8 DEB orbits at an average altitude of 1,555 km in the uppermost reaches of Low Earth Orbit. At this altitude, orbital decay is effectively zero without active deorbiting, and coverage footprints are significantly larger than lower LEO, though at the cost of higher latency. Within ±50 km of SL-8 DEB’s average altitude, there are currently 34 active payloads and 221 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 73.9°, SL-8 DEB passes over latitudes between 73.9°N and 73.9°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 20 share a similar altitude band with SL-8 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-8 DEB orbits in Low Earth Orbit (LEO) at altitudes between 1,439 km (perigee) and 1,671 km (apogee), with an average altitude of approximately 1,555 km. It completes one orbit every 117 minutes, travelling at approximately 25,530 km/h (15,863 mph).
SL-8 DEB (NORAD ID 21175) 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-8 DEB was launched on 1991-02-12 from PKMTR. At its current altitude, the estimated remaining orbital lifetime is: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks SL-8 DEB (NORAD ID 21175) 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-8 DEB travels at approximately 25,530 km/h (15,863 mph) — roughly 7.09 km/s. It completes 12.29 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 25 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 7.09 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-8 DEB. Read more about debris statistics and the Kessler syndrome.