COSMOS 1124 DEB
NORAD 32982
Debris
MEO
1979-077H
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MEO · NORAD 32982
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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
2120 km
Apogee
36669 km
Inclination
65.4°
Period
686.3 min
Mean Motion
2.09825527 rev/day
TLE Epoch
2026-06-21 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude19,395 km
Orbital Velocity14,160 km/h
Velocity3.93 km/s
Orbital Period11 hours 26 minutes
Orbits / Day2.10
Eccentricity0.6705
Semi-Major Axis25,766 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1979-08-28
Launch Site
PKMTR
Int'l Designator
1979-077H
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
COSMOS 1124 DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 1979-08-28 from PKMTR on the Oko launch. With over 47 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 2,120 km and 36,669 km with an inclination of 65.4°. It travels at approximately 14,160 km/h (3.93 km/s), completing one full orbit every 11 hours 26 minutes — that’s roughly 2.10 orbits per day. Its orbital eccentricity of 0.6705 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. As orbital debris, COSMOS 1124 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 1124 DEB orbits at an average altitude of 19,395 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 1124 DEB’s average altitude, there are currently 0 active payloads and 13 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 65.4°, COSMOS 1124 DEB passes over latitudes between 65.4°N and 65.4°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 1,287 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 1124 DEB orbits in Medium Earth Orbit (MEO) at altitudes between 2,120 km (perigee) and 36,669 km (apogee), with an average altitude of approximately 19,395 km. It completes one orbit every 11 hours 26 minutes, travelling at approximately 14,160 km/h (8,798 mph).
COSMOS 1124 DEB (NORAD ID 32982) 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 1124 DEB was launched on 1979-08-28 from PKMTR. View the full satellite launch log.
Yes — Orbital Radar tracks COSMOS 1124 DEB (NORAD ID 32982) 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 1124 DEB travels at approximately 14,160 km/h (8,798 mph) — roughly 3.93 km/s. It completes 2.10 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 3.93 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 1124 DEB. Read more about debris statistics and the Kessler syndrome.