SL-8 DEB
NORAD 21212
Debris
LEO
1991-009BF
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LEO · NORAD 21212
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
1464 km
Apogee
1836 km
Inclination
74.2°
Period
119.3 min
Mean Motion
12.06928849 rev/day
TLE Epoch
2026-06-16 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,650 km
Orbital Velocity25,378 km/h
Velocity7.05 km/s
Orbital Period119 minutes
Orbits / Day12.07
Eccentricity0.0232
Semi-Major Axis8,021 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1991-02-12
Launch Site
PKMTR
Int'l Designator
1991-009BF
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 1,464 km and 1,836 km with an inclination of 74.2°. It travels at approximately 25,378 km/h (7.05 km/s), completing one full orbit every 119 minutes — that’s roughly 12.07 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 1,650 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 23 active payloads and 111 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 74.2°, SL-8 DEB passes over latitudes between 74.2°N and 74.2°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 1,287 active satellites in total, of which 11 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 1,464 km (perigee) and 1,836 km (apogee), with an average altitude of approximately 1,650 km. It completes one orbit every 119 minutes, travelling at approximately 25,378 km/h (15,769 mph).
SL-8 DEB (NORAD ID 21212) 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 21212) 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 25,378 km/h (15,769 mph) — roughly 7.05 km/s. It completes 12.07 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 24 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 7.05 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.