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COSMOS 1285 DEB

NORAD 12993 Debris MEO 1981-071E
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
3158 km
Apogee
37687 km
Inclination
67.2°
Period
727.8 min
Mean Motion
1.97870126 rev/day
TLE Epoch
2026-06-19 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude20,423 km
Orbital Velocity13,885 km/h
Velocity3.86 km/s
Orbital Period12 hours 8 minutes
Orbits / Day1.98
Eccentricity0.6444
Semi-Major Axis26,794 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1981-08-04
Launch Site
PKMTR
Int'l Designator
1981-071E
Object Type
Debris
RCS Size
Large (>1 m²)
📖 About This Object
COSMOS 1285 DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 1981-08-04 from PKMTR. With over 45 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 3,158 km and 37,687 km with an inclination of 67.2°. It travels at approximately 13,885 km/h (3.86 km/s), completing one full orbit every 12 hours 8 minutes — that’s roughly 1.98 orbits per day. Its orbital eccentricity of 0.6444 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. As orbital debris, COSMOS 1285 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
COSMOS 1285 DEB orbits at an average altitude of 20,423 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 COSMOS 1285 DEB’s average altitude, there are currently 2 active payloads and 12 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 67.2°, COSMOS 1285 DEB passes over latitudes between 67.2°N and 67.2°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.
🔗 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
COSMOS 1285 DEB orbits in Medium Earth Orbit (MEO) at altitudes between 3,158 km (perigee) and 37,687 km (apogee), with an average altitude of approximately 20,423 km. It completes one orbit every 12 hours 8 minutes, travelling at approximately 13,885 km/h (8,628 mph).
COSMOS 1285 DEB (NORAD ID 12993) 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.
COSMOS 1285 DEB was launched on 1981-08-04 from PKMTR. View the full satellite launch log.
Yes — Orbital Radar tracks COSMOS 1285 DEB (NORAD ID 12993) 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.
COSMOS 1285 DEB travels at approximately 13,885 km/h (8,628 mph) — roughly 3.86 km/s. It completes 1.98 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 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 3.86 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 COSMOS 1285 DEB. Read more about debris statistics and the Kessler syndrome.