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SL-8 DEB *

NORAD 14818 Debris LEO 1977-059D
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
483 km
Apogee
489 km
Inclination
74.0°
Period
94.3 min
Mean Motion
15.26558791 rev/day
TLE Epoch
2026-06-19 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude486 km
Orbital Velocity27,448 km/h
Velocity7.62 km/s
Orbital Period94 minutes
Orbits / Day15.27
Eccentricity0.0004
Semi-Major Axis6,857 km
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1977-07-01
Launch Site
PKMTR
Int'l Designator
1977-059D
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 1977-07-01 from PKMTR on the Strela-2M launch. With over 49 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 483 km and 489 km with an inclination of 74.0°. It travels at approximately 27,448 km/h (7.62 km/s), completing one full orbit every 94 minutes — that’s roughly 15.27 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 ~1–3 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 486 km in the core of Low Earth Orbit, the most heavily utilised altitude band. The balance of moderate drag (limiting debris accumulation) and short signal path (enabling low-latency links and high-resolution imaging) makes this regime the default for most commercial and government missions. Within ±50 km of SL-8 DEB *’s average altitude, there are currently 8,109 active payloads and 224 tracked debris or rocket body fragments — notable neighbours include STARLINK-1017, STARLINK-1039, STARLINK-1047. This makes it one of the more crowded altitude bands, containing roughly 46.5% 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 51 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 483 km (perigee) and 489 km (apogee), with an average altitude of approximately 486 km. It completes one orbit every 94 minutes, travelling at approximately 27,448 km/h (17,055 mph).
SL-8 DEB * (NORAD ID 14818) 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 1977-07-01 from PKMTR. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks SL-8 DEB * (NORAD ID 14818) 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 27,448 km/h (17,055 mph) — roughly 7.62 km/s. It completes 15.27 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 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 7.62 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.