Skip to content
Home Library Satellite Directory SL-8 DEB

SL-8 DEB

NORAD 60605 Debris LEO 1991-009EA
CONNECTING… LEO · NORAD 60605
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
1453 km
Apogee
1732 km
Inclination
74.0°
Period
118.0 min
Mean Motion
12.19936625 rev/day
TLE Epoch
2026-06-20 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,593 km
Orbital Velocity25,469 km/h
Velocity7.07 km/s
Orbital Period118 minutes
Orbits / Day12.20
Eccentricity0.0175
Semi-Major Axis7,964 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1991-02-12
Launch Site
PKMTR
Int'l Designator
1991-009EA
Object Type
Debris
RCS Size
Small (<0.1 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 on the Strela-1M launch. With over 35 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 1,453 km and 1,732 km with an inclination of 74.0°. It travels at approximately 25,469 km/h (7.07 km/s), completing one full orbit every 118 minutes — that’s roughly 12.20 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 1,593 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 33 active payloads and 210 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 74.0°, 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 1,285 active satellites in total, of which 18 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 1,453 km (perigee) and 1,732 km (apogee), with an average altitude of approximately 1,593 km. It completes one orbit every 118 minutes, travelling at approximately 25,469 km/h (15,826 mph).
SL-8 DEB (NORAD ID 60605) 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 60605) 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 25,469 km/h (15,826 mph) — roughly 7.07 km/s. It completes 12.20 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 7.07 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.