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SL-16 DEB

NORAD 25401 Debris LEO 1998-043H
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🛰️ Orbital Parameters
Perigee
795 km
Apogee
1028 km
Inclination
98.5°
Period
103.2 min
Mean Motion
13.94842568 rev/day
TLE Epoch
2026-06-20 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude912 km
Orbital Velocity26,634 km/h
Velocity7.40 km/s
Orbital Period103 minutes
Orbits / Day13.95
Eccentricity0.0160
Semi-Major Axis7,283 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1998-07-10
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1998-043H
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 1998-07-10 from Baikonur, Kazakhstan on the Resurs-O1 No. 4L launch. With over 28 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 795 km and 1,028 km with an inclination of 98.5°. It travels at approximately 26,634 km/h (7.40 km/s), completing one full orbit every 103 minutes — that’s roughly 13.95 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 ~100–500 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 912 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 222 active payloads and 1,206 tracked debris or rocket body fragments. With an inclination of 98.5°, SL-16 DEB passes over latitudes between 98.5°N and 98.5°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 50 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 912 km altitude. Its 98.5° 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 103 minutes, travelling at 26,634 km/h.
SL-16 DEB (NORAD ID 25401) 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 1998-07-10 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: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks SL-16 DEB (NORAD ID 25401) 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 26,634 km/h (16,549 mph) — roughly 7.40 km/s. It completes 13.95 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 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 7.40 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.