COSMOS 1691 DEB
NORAD 16272
Debris
LEO
1985-094R
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LEO · NORAD 16272
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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
1328 km
Apogee
1393 km
Inclination
82.6°
Period
112.9 min
Mean Motion
12.75297296 rev/day
TLE Epoch
2026-06-15 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,361 km
Orbital Velocity25,849 km/h
Velocity7.18 km/s
Orbital Period113 minutes
Orbits / Day12.75
Eccentricity0.0042
Semi-Major Axis7,732 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1985-10-09
Launch Site
PKMTR
Int'l Designator
1985-094R
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
COSMOS 1691 DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 1985-10-09 from PKMTR. With over 41 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 1,328 km and 1,393 km with an inclination of 82.6°. It travels at approximately 25,849 km/h (7.18 km/s), completing one full orbit every 113 minutes — that’s roughly 12.75 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. As orbital debris, COSMOS 1691 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 1691 DEB orbits at an average altitude of 1,361 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 COSMOS 1691 DEB’s average altitude, there are currently 101 active payloads and 144 tracked debris or rocket body fragments. With an inclination of 82.6°, COSMOS 1691 DEB passes over latitudes between 82.6°N and 82.6°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. Russia (CIS) operates approximately 1,286 active satellites in total, of which 87 share a similar altitude band with COSMOS 1691 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
COSMOS 1691 DEB orbits in Low Earth Orbit (LEO) at altitudes between 1,328 km (perigee) and 1,393 km (apogee), with an average altitude of approximately 1,361 km. It completes one orbit every 113 minutes, travelling at approximately 25,849 km/h (16,062 mph).
COSMOS 1691 DEB (NORAD ID 16272) 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 1691 DEB was launched on 1985-10-09 from PKMTR. At its current altitude, the estimated remaining orbital lifetime is: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks COSMOS 1691 DEB (NORAD ID 16272) 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 1691 DEB travels at approximately 25,849 km/h (16,062 mph) — roughly 7.18 km/s. It completes 12.75 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 26 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 7.18 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 1691 DEB. Read more about debris statistics and the Kessler syndrome.