COSMOS 1191 DEB
NORAD 27897
Debris
HEO
1980-057K
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HEO · NORAD 27897
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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
580 km
Apogee
40015 km
Inclination
62.3°
Period
722.7 min
Mean Motion
1.99265962 rev/day
TLE Epoch
2026-11-03 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude20,298 km
Orbital Velocity13,918 km/h
Velocity3.87 km/s
Orbital Period12 hours 3 minutes
Orbits / Day1.99
Eccentricity0.7394
Semi-Major Axis26,669 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1980-07-02
Launch Site
Plesetsk Cosmodrome, Russia
Int'l Designator
1980-057K
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
COSMOS 1191 DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 1980-07-02 from Plesetsk Cosmodrome, Russia on the Oko launch. With over 46 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 580 km and 40,015 km with an inclination of 62.3°. It travels at approximately 13,918 km/h (3.87 km/s), completing one full orbit every 12 hours 3 minutes — that’s roughly 1.99 orbits per day. Its orbital eccentricity of 0.7394 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. As orbital debris, COSMOS 1191 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 1191 DEB follows a Highly Elliptical Orbit, sweeping between 580 km (perigee) and 40,015 km (apogee). It spends most of its 12 hours 3 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 1191 DEB’s average altitude, there are currently 3 active payloads and 15 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 62.3°, COSMOS 1191 DEB passes over latitudes between 62.3°N and 62.3°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 1,569 active satellites in total, of which 3 share a similar altitude band with COSMOS 1191 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 1191 DEB follows a Highly Elliptical Orbit, swinging between 580 km (perigee) and 40,015 km (apogee). It spends most of its 12 hours 3 minutes orbital period near apogee, moving slowly at high altitude — effectively loitering over a region of interest before rapidly sweeping through perigee.
COSMOS 1191 DEB (NORAD ID 27897) 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 1191 DEB was launched on 1980-07-02 from Plesetsk Cosmodrome, Russia, Russia’s northern military cosmodrome, used primarily for high-inclination and polar orbit launches. 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 1191 DEB (NORAD ID 27897) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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 1191 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 13,918 km/h (3.87 km/s), completing one revolution every 12 hours 3 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 3.87 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 1191 DEB. Read more about debris statistics and the Kessler syndrome.