SL-8 DEB
NORAD 1590
Debris
LEO
1965-073G
CONNECTING…
LEO · NORAD 1590
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
1331 km
Apogee
1600 km
Inclination
56.1°
Period
115.2 min
Mean Motion
12.49814569 rev/day
TLE Epoch
2026-09-16 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,466 km
Orbital Velocity25,675 km/h
Velocity7.13 km/s
Orbital Period115 minutes
Orbits / Day12.50
Eccentricity0.0172
Semi-Major Axis7,837 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1965-09-18
Launch Site
Baikonur Cosmodrome, Kazakhstan
Int'l Designator
1965-073G
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
SL-8 DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 1965-09-18 from Baikonur Cosmodrome, Kazakhstan on the Strela-1 launch. After more than 61 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Low Earth Orbit (LEO) at altitudes between 1,331 km and 1,600 km with an inclination of 56.1°. It travels at approximately 25,675 km/h (7.13 km/s), completing one full orbit every 115 minutes — that’s roughly 12.50 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. As orbital debris, SL-8 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-8 DEB orbits at an average altitude of 1,466 km in the uppermost reaches of Low Earth Orbit. At this altitude, orbital decay is effectively zero without active deorbiting, and coverage footprints are significantly larger than lower LEO, though at the cost of higher latency. Within ±50 km of SL-8 DEB’s average altitude, there are currently 465 active payloads and 367 tracked debris or rocket body fragments. With an inclination of 56.1°, SL-8 DEB passes over latitudes between 56.1°N and 56.1°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 1,537 active satellites in total, of which 440 share a similar altitude band with SL-8 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-8 DEB orbits in Low Earth Orbit (LEO) at altitudes between 1,331 km (perigee) and 1,600 km (apogee), with an average altitude of approximately 1,466 km. It completes one orbit every 115 minutes, travelling at approximately 25,675 km/h (15,954 mph).
SL-8 DEB (NORAD ID 1590) 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-8 DEB was launched on 1965-09-18 from Baikonur Cosmodrome, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. At its current altitude, the estimated remaining orbital lifetime is: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks SL-8 DEB (NORAD ID 1590) 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-8 DEB travels at approximately 25,675 km/h (15,954 mph) — roughly 7.13 km/s. It completes 12.50 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 25 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 7.13 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-8 DEB. Read more about debris statistics and the Kessler syndrome.