SL-12 DEB
NORAD 44588
Debris
MEO
1999-027E
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MEO · NORAD 44588
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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
16148 km
Apogee
36737 km
Inclination
7.3°
Period
986.2 min
Mean Motion
1.46010867 rev/day
TLE Epoch
2026-06-16 13:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude26,443 km
Orbital Velocity12,547 km/h
Velocity3.49 km/s
Orbital Period16 hours 26 minutes
Orbits / Day1.46
Eccentricity0.3137
Semi-Major Axis32,814 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1999-05-20
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1999-027E
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
SL-12 DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 1999-05-20 from Baikonur, Kazakhstan on the Telesat DTH-1 launch. With over 27 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 16,148 km and 36,737 km with an inclination of 7.3°. It travels at approximately 12,547 km/h (3.49 km/s), completing one full orbit every 16 hours 26 minutes — that’s roughly 1.46 orbits per day. Its orbital eccentricity of 0.3137 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. As orbital debris, SL-12 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-12 DEB orbits at an average altitude of 26,443 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-12 DEB’s average altitude, there are currently 0 active payloads and 3 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 7.3°, SL-12 DEB passes over latitudes between 7.3°N and 7.3°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. Russia (CIS) operates approximately 1,285 active satellites in total.
🔗 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-12 DEB orbits in Medium Earth Orbit (MEO) at altitudes between 16,148 km (perigee) and 36,737 km (apogee), with an average altitude of approximately 26,443 km. It completes one orbit every 16 hours 26 minutes, travelling at approximately 12,547 km/h (7,796 mph).
SL-12 DEB (NORAD ID 44588) 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-12 DEB was launched on 1999-05-20 from Baikonur, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. View the full satellite launch log.
Yes — Orbital Radar tracks SL-12 DEB (NORAD ID 44588) 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-12 DEB travels at approximately 12,547 km/h (7,796 mph) — roughly 3.49 km/s. It completes 1.46 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 3 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 3.49 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-12 DEB. Read more about debris statistics and the Kessler syndrome.