COSMOS 1934 DEB
NORAD 22919
Debris
LEO
1988-023D
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LEO · NORAD 22919
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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
888 km
Apogee
934 km
Inclination
83.0°
Period
103.2 min
Mean Motion
13.95049725 rev/day
TLE Epoch
2026-06-19 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude911 km
Orbital Velocity26,635 km/h
Velocity7.40 km/s
Orbital Period103 minutes
Orbits / Day13.95
Eccentricity0.0032
Semi-Major Axis7,282 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1988-03-22
Launch Site
PKMTR
Int'l Designator
1988-023D
Object Type
Debris
RCS Size
Small (<0.1 m²)
📖 About This Object
COSMOS 1934 DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 1988-03-22 from PKMTR. With over 38 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 888 km and 934 km with an inclination of 83.0°. It travels at approximately 26,635 km/h (7.40 km/s), completing one full orbit every 103 minutes — that’s roughly 13.95 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. As orbital debris, COSMOS 1934 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 1934 DEB orbits at an average altitude of 911 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 1934 DEB’s average altitude, there are currently 217 active payloads and 1,224 tracked debris or rocket body fragments. With an inclination of 83.0°, COSMOS 1934 DEB passes over latitudes between 83.0°N and 83.0°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 50 share a similar altitude band with COSMOS 1934 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 1934 DEB orbits in Low Earth Orbit (LEO) at altitudes between 888 km (perigee) and 934 km (apogee), with an average altitude of approximately 911 km. It completes one orbit every 103 minutes, travelling at approximately 26,635 km/h (16,550 mph).
COSMOS 1934 DEB (NORAD ID 22919) 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 1934 DEB was launched on 1988-03-22 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 1934 DEB (NORAD ID 22919) 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 1934 DEB travels at approximately 26,635 km/h (16,550 mph) — roughly 7.40 km/s. It completes 13.95 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 7.40 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 1934 DEB. Read more about debris statistics and the Kessler syndrome.