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SL-19 DEB

NORAD 23485 Debris MEO 1994-085H
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
1892 km
Apogee
2129 km
Inclination
64.7°
Period
127.4 min
Mean Motion
11.29917807 rev/day
TLE Epoch
2026-06-20 09:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude2,011 km
Orbital Velocity24,826 km/h
Velocity6.90 km/s
Orbital Period2 hours 7 minutes
Orbits / Day11.30
Eccentricity0.0141
Semi-Major Axis8,382 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1994-12-26
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1994-085H
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
SL-19 DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 1994-12-26 from Baikonur, Kazakhstan on the Radio-ROSTO launch. With over 32 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 1,892 km and 2,129 km with an inclination of 64.7°. It travels at approximately 24,826 km/h (6.90 km/s), completing one full orbit every 2 hours 7 minutes — that’s roughly 11.30 orbits per day. As orbital debris, SL-19 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-19 DEB orbits at an average altitude of 2,011 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of SL-19 DEB’s average altitude, there are currently 8 active payloads and 26 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 64.7°, SL-19 DEB passes over latitudes between 64.7°N and 64.7°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 1,285 active satellites in total, of which 2 share a similar altitude band with SL-19 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-19 DEB orbits in Medium Earth Orbit (MEO) at altitudes between 1,892 km (perigee) and 2,129 km (apogee), with an average altitude of approximately 2,011 km. It completes one orbit every 2 hours 7 minutes, travelling at approximately 24,826 km/h (15,426 mph).
SL-19 DEB (NORAD ID 23485) 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-19 DEB was launched on 1994-12-26 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: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks SL-19 DEB (NORAD ID 23485) 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-19 DEB travels at approximately 24,826 km/h (15,426 mph) — roughly 6.90 km/s. It completes 11.30 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 23 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 6.90 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-19 DEB. Read more about debris statistics and the Kessler syndrome.