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SL-16 DEB

NORAD 22392 Debris LEO 1992-093CH
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Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
546 km
Apogee
651 km
Inclination
70.9°
Period
96.7 min
Mean Motion
14.89691496 rev/day
TLE Epoch
2026-06-26 02:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude599 km
Orbital Velocity27,225 km/h
Velocity7.56 km/s
Orbital Period97 minutes
Orbits / Day14.90
Eccentricity0.0075
Semi-Major Axis6,970 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
1992-093CH
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 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 546 km and 651 km with an inclination of 70.9°. It travels at approximately 27,225 km/h (7.56 km/s), completing one full orbit every 97 minutes — that’s roughly 14.90 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 599 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 2,114 active payloads and 648 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3005, STARLINK-3090. This makes it one of the more crowded altitude bands, containing roughly 12.1% of all active satellites. With an inclination of 70.9°, SL-16 DEB passes over latitudes between 70.9°N and 70.9°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 25 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 546 km (perigee) and 651 km (apogee), with an average altitude of approximately 599 km. It completes one orbit every 97 minutes, travelling at approximately 27,225 km/h (16,917 mph).
SL-16 DEB (NORAD ID 22392) 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 22392) 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 27,225 km/h (16,917 mph) — roughly 7.56 km/s. It completes 14.90 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 7.56 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.