COSMOS 2528 DEB
NORAD 45037
Debris
LEO
2018-082C
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LEO · NORAD 45037
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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
886 km
Apogee
905 km
Inclination
67.2°
Period
102.9 min
Mean Motion
13.99509611 rev/day
TLE Epoch
2026-06-19 12:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude896 km
Orbital Velocity26,663 km/h
Velocity7.41 km/s
Orbital Period103 minutes
Orbits / Day14.00
Eccentricity0.0013
Semi-Major Axis7,267 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2018-10-25
Launch Site
PKMTR
Int'l Designator
2018-082C
Object Type
Debris
RCS Size
Large (>1 m²)
📖 About This Object
COSMOS 2528 DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 2018-10-25 from PKMTR. It orbits in Low Earth Orbit (LEO) at altitudes between 886 km and 905 km with an inclination of 67.2°. It travels at approximately 26,663 km/h (7.41 km/s), completing one full orbit every 103 minutes — that’s roughly 14.00 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. As orbital debris, COSMOS 2528 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 2528 DEB orbits at an average altitude of 896 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of COSMOS 2528 DEB’s average altitude, there are currently 197 active payloads and 1,422 tracked debris or rocket body fragments. With an inclination of 67.2°, COSMOS 2528 DEB passes over latitudes between 67.2°N and 67.2°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, of which 57 share a similar altitude band with COSMOS 2528 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 2528 DEB orbits in Low Earth Orbit (LEO) at altitudes between 886 km (perigee) and 905 km (apogee), with an average altitude of approximately 896 km. It completes one orbit every 103 minutes, travelling at approximately 26,663 km/h (16,568 mph).
COSMOS 2528 DEB (NORAD ID 45037) 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 2528 DEB was launched on 2018-10-25 from PKMTR. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks COSMOS 2528 DEB (NORAD ID 45037) 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 2528 DEB travels at approximately 26,663 km/h (16,568 mph) — roughly 7.41 km/s. It completes 14.00 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 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 7.41 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 2528 DEB. Read more about debris statistics and the Kessler syndrome.