SL-14 DEB
NORAD 19580
Debris
LEO
1978-100AL
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LEO · NORAD 19580
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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
1198 km
Apogee
1675 km
Inclination
82.7°
Period
114.6 min
Mean Motion
12.56650750 rev/day
TLE Epoch
2026-06-12 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,437 km
Orbital Velocity25,723 km/h
Velocity7.15 km/s
Orbital Period115 minutes
Orbits / Day12.57
Eccentricity0.0305
Semi-Major Axis7,808 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1978-10-26
Launch Site
PKMTR
Int'l Designator
1978-100AL
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
SL-14 DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 1978-10-26 from PKMTR on the Meteor-2 GVM 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 1,198 km and 1,675 km with an inclination of 82.7°. It travels at approximately 25,723 km/h (7.15 km/s), completing one full orbit every 115 minutes — that’s roughly 12.57 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. As orbital debris, SL-14 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-14 DEB orbits at an average altitude of 1,437 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-14 DEB’s average altitude, there are currently 366 active payloads and 180 tracked debris or rocket body fragments. With an inclination of 82.7°, SL-14 DEB passes over latitudes between 82.7°N and 82.7°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. Russia (CIS) operates approximately 1,285 active satellites in total, of which 331 share a similar altitude band with SL-14 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-14 DEB orbits in Low Earth Orbit (LEO) at altitudes between 1,198 km (perigee) and 1,675 km (apogee), with an average altitude of approximately 1,437 km. It completes one orbit every 115 minutes, travelling at approximately 25,723 km/h (15,983 mph).
SL-14 DEB (NORAD ID 19580) 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-14 DEB was launched on 1978-10-26 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-14 DEB (NORAD ID 19580) 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-14 DEB travels at approximately 25,723 km/h (15,983 mph) — roughly 7.15 km/s. It completes 12.57 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 25 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 7.15 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-14 DEB. Read more about debris statistics and the Kessler syndrome.