SL-8 DEB *
NORAD 18501
Debris
LEO
1978-019E
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LEO · NORAD 18501
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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
625 km
Apogee
640 km
Inclination
74.0°
Period
97.4 min
Mean Motion
14.79084654 rev/day
TLE Epoch
2026-06-20 08:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude633 km
Orbital Velocity27,159 km/h
Velocity7.54 km/s
Orbital Period97 minutes
Orbits / Day14.79
Eccentricity0.0011
Semi-Major Axis7,004 km
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1978-02-17
Launch Site
PKMTR
Int'l Designator
1978-019E
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 1978-02-17 from PKMTR on the Strela-2M launch. With over 48 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 625 km and 640 km with an inclination of 74.0°. It travels at approximately 27,159 km/h (7.54 km/s), completing one full orbit every 97 minutes — that’s roughly 14.79 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 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 633 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 779 active payloads and 862 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050. 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 10 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 625 km (perigee) and 640 km (apogee), with an average altitude of approximately 633 km. It completes one orbit every 97 minutes, travelling at approximately 27,159 km/h (16,876 mph).
SL-8 DEB * (NORAD ID 18501) 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 1978-02-17 from PKMTR. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks SL-8 DEB * (NORAD ID 18501) 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 27,159 km/h (16,876 mph) — roughly 7.54 km/s. It completes 14.79 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 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 7.54 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.