SL-8 DEB
NORAD 1480
Debris
MEO
1965-020BE
CONNECTING…
MEO · NORAD 1480
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
759 km
Apogee
2050 km
Inclination
56.1°
Period
113.9 min
Mean Motion
12.64498933 rev/day
TLE Epoch
2026-09-19 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,405 km
Orbital Velocity25,776 km/h
Velocity7.16 km/s
Orbital Period114 minutes
Orbits / Day12.64
Eccentricity0.0830
Semi-Major Axis7,776 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1965-03-15
Launch Site
Baikonur Cosmodrome, Kazakhstan
Int'l Designator
1965-020BE
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 1965-03-15 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 Medium Earth Orbit (MEO) at altitudes between 759 km and 2,050 km with an inclination of 56.1°. It travels at approximately 25,776 km/h (7.16 km/s), completing one full orbit every 114 minutes — that’s roughly 12.64 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 1,405 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-8 DEB’s average altitude, there are currently 355 active payloads and 273 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 297 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 Medium Earth Orbit (MEO) at altitudes between 759 km (perigee) and 2,050 km (apogee), with an average altitude of approximately 1,405 km. It completes one orbit every 114 minutes, travelling at approximately 25,776 km/h (16,016 mph).
SL-8 DEB (NORAD ID 1480) 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 1965-03-15 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 1480) 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 25,776 km/h (16,016 mph) — roughly 7.16 km/s. It completes 12.64 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 7.16 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.