SL-16 DEB
NORAD 22296
Debris
LEO
1992-093L
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LEO · NORAD 22296
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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
549 km
Apogee
586 km
Inclination
70.8°
Period
96.0 min
Mean Motion
14.99807747 rev/day
TLE Epoch
2026-06-26 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude568 km
Orbital Velocity27,286 km/h
Velocity7.58 km/s
Orbital Period96 minutes
Orbits / Day15.00
Eccentricity0.0027
Semi-Major Axis6,939 km
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1992-12-25
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1992-093L
Object Type
Debris
RCS Size
Small (<0.1 m²)
📖 About This Object
SL-16 DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 1992-12-25 from Baikonur, Kazakhstan on the Tselina-2 launch. With over 34 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 549 km and 586 km with an inclination of 70.8°. It travels at approximately 27,286 km/h (7.58 km/s), completing one full orbit every 96 minutes — that’s roughly 15.00 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 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 568 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-16 DEB’s average altitude, there are currently 2,973 active payloads and 475 tracked debris or rocket body fragments — notable neighbours include STARLINK-1184, STARLINK-1276, ONEWEB-0050. This makes it one of the more crowded altitude bands, containing roughly 17% of all active satellites. With an inclination of 70.8°, SL-16 DEB passes over latitudes between 70.8°N and 70.8°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 1,286 active satellites in total, of which 31 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 orbits in Low Earth Orbit (LEO) at altitudes between 549 km (perigee) and 586 km (apogee), with an average altitude of approximately 568 km. It completes one orbit every 96 minutes, travelling at approximately 27,286 km/h (16,955 mph).
SL-16 DEB (NORAD ID 22296) 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 1992-12-25 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: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks SL-16 DEB (NORAD ID 22296) 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 27,286 km/h (16,955 mph) — roughly 7.58 km/s. It completes 15.00 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 7.58 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.