SL-16 DEB
NORAD 25865
Debris
LEO
1999-039F
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LEO · NORAD 25865
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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
641 km
Apogee
896 km
Inclination
97.8°
Period
100.2 min
Mean Motion
14.36993341 rev/day
TLE Epoch
2026-06-20 08:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude769 km
Orbital Velocity26,899 km/h
Velocity7.47 km/s
Orbital Period100 minutes
Orbits / Day14.37
Eccentricity0.0179
Semi-Major Axis7,140 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1999-07-17
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1999-039F
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
SL-16 DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 1999-07-17 from Baikonur, Kazakhstan on the Okean-O No. 1 launch. With over 27 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 641 km and 896 km with an inclination of 97.8°. It travels at approximately 26,899 km/h (7.47 km/s), completing one full orbit every 100 minutes — that’s roughly 14.37 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. As orbital debris, SL-16 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-16 DEB orbits at an average altitude of 769 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of SL-16 DEB’s average altitude, there are currently 387 active payloads and 2,067 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0179, ONEWEB-0455. With an inclination of 97.8°, SL-16 DEB passes over latitudes between 97.8°N and 97.8°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 55 share a similar altitude band with SL-16 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-16 DEB is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 769 km altitude. Its 97.8° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 100 minutes, travelling at 26,899 km/h.
SL-16 DEB (NORAD ID 25865) 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-16 DEB was launched on 1999-07-17 from Baikonur, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks SL-16 DEB (NORAD ID 25865) 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-16 DEB travels at approximately 26,899 km/h (16,714 mph) — roughly 7.47 km/s. It completes 14.37 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 7.47 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-16 DEB. Read more about debris statistics and the Kessler syndrome.