SL-8 DEB
NORAD 23007
Debris
LEO
1993-036C
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LEO · NORAD 23007
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
724 km
Apogee
737 km
Inclination
74.0°
Period
99.4 min
Mean Motion
14.48564067 rev/day
TLE Epoch
2026-06-26 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude731 km
Orbital Velocity26,971 km/h
Velocity7.49 km/s
Orbital Period99 minutes
Orbits / Day14.49
Eccentricity0.0009
Semi-Major Axis7,102 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1993-06-16
Launch Site
PKMTR
Int'l Designator
1993-036C
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 1993-06-16 from PKMTR on the Strela-2M launch. With over 33 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 724 km and 737 km with an inclination of 74.0°. It travels at approximately 26,971 km/h (7.49 km/s), completing one full orbit every 99 minutes — that’s roughly 14.49 orbits per day. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 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 731 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-8 DEB’s average altitude, there are currently 359 active payloads and 1,859 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, LANDSAT 9. With an inclination of 74.0°, SL-8 DEB passes over latitudes between 74.0°N and 74.0°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 38 share a similar altitude band with SL-8 DEB.
🔗 Cosmos–Iridium Collision Debris
This debris object was created by the first accidental hypervelocity collision between two intact satellites — Cosmos 2251 (defunct, Russia) and Iridium 33 (active, USA) — on 10 February 2009 at approximately 790 km altitude. The collision occurred at a relative velocity of about 11.7 km/s and produced over 2,300 trackable fragments, many of which remain in orbit.
❓ Frequently Asked Questions
SL-8 DEB orbits in Low Earth Orbit (LEO) at altitudes between 724 km (perigee) and 737 km (apogee), with an average altitude of approximately 731 km. It completes one orbit every 99 minutes, travelling at approximately 26,971 km/h (16,759 mph).
SL-8 DEB (NORAD ID 23007) 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 1993-06-16 from PKMTR. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks SL-8 DEB (NORAD ID 23007) 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 26,971 km/h (16,759 mph) — roughly 7.49 km/s. It completes 14.49 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 7.49 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.