COSMOS 1285 DEB
NORAD 26680
Debris
HEO
1981-071L
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HEO · NORAD 26680
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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
529 km
Apogee
40221 km
Inclination
63.0°
Period
725.8 min
Mean Motion
1.98395035 rev/day
TLE Epoch
2026-06-19 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude20,375 km
Orbital Velocity13,898 km/h
Velocity3.86 km/s
Orbital Period12 hours 6 minutes
Orbits / Day1.98
Eccentricity0.7420
Semi-Major Axis26,746 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
1981-071L
Object Type
Debris
RCS Size
Medium (0.1–1 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 Highly Elliptical Orbit (HEO) at altitudes between 529 km and 40,221 km with an inclination of 63.0°. It travels at approximately 13,898 km/h (3.86 km/s), completing one full orbit every 12 hours 6 minutes — that’s roughly 1.98 orbits per day. Its orbital eccentricity of 0.7420 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 follows a Highly Elliptical Orbit, sweeping between 529 km (perigee) and 40,221 km (apogee). It spends most of its 12 hours 6 minutes orbital period near apogee, effectively loitering over a region of interest before rapidly sweeping through perigee — a profile used for high-latitude communications (Molniya orbits), early-warning systems and magnetospheric science. Within ±50 km of COSMOS 1285 DEB’s average altitude, there are currently 2 active payloads and 7 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 63.0°, COSMOS 1285 DEB passes over latitudes between 63.0°N and 63.0°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 follows a Highly Elliptical Orbit, swinging between 529 km (perigee) and 40,221 km (apogee). It spends most of its 12 hours 6 minutes orbital period near apogee, moving slowly at high altitude — effectively loitering over a region of interest before rapidly sweeping through perigee.
COSMOS 1285 DEB (NORAD ID 26680) 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. 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 COSMOS 1285 DEB (NORAD ID 26680) 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’s speed varies dramatically throughout its orbit. At perigee it moves at its fastest, and at apogee it slows to a fraction of that — this is Kepler’s second law in action. Its average orbital velocity is approximately 13,898 km/h (3.86 km/s), completing one revolution every 12 hours 6 minutes. Learn more about highly elliptical orbits.
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.