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COSMOS 1124 DEB

NORAD 32982 Debris MEO 1979-077H
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
2110 km
Apogee
36681 km
Inclination
65.4°
Period
686.3 min
Mean Motion
2.09820118 rev/day
TLE Epoch
2026-06-14 08:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude19,396 km
Orbital Velocity14,159 km/h
Velocity3.93 km/s
Orbital Period11 hours 26 minutes
Orbits / Day2.10
Eccentricity0.6709
Semi-Major Axis25,767 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. With over 47 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 2,110 km and 36,681 km with an inclination of 65.4°. It travels at approximately 14,159 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 0.6709 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 19,396 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 1,286 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 1124 DEB orbits in Medium Earth Orbit (MEO) at altitudes between 2,110 km (perigee) and 36,681 km (apogee), with an average altitude of approximately 19,396 km. It completes one orbit every 11 hours 26 minutes, travelling at approximately 14,159 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 14,159 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.