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METEOR 2-5 DEB

NORAD 38275 Debris LEO 1979-095BV
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
570 km
Apogee
581 km
Inclination
81.1°
Period
96.2 min
Mean Motion
14.97152534 rev/day
TLE Epoch
2026-06-11 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude576 km
Orbital Velocity27,270 km/h
Velocity7.58 km/s
Orbital Period96 minutes
Orbits / Day14.97
Eccentricity0.0008
Semi-Major Axis6,947 km
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1979-10-31
Launch Site
PKMTR
Int'l Designator
1979-095BV
Object Type
Debris
RCS Size
Small (<0.1 m²)
📖 About This Object
METEOR 2-5 DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 1979-10-31 from PKMTR on the Meteor-2 No. 7 launch. With over 47 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 570 km and 581 km with an inclination of 81.1°. It travels at approximately 27,270 km/h (7.58 km/s), completing one full orbit every 96 minutes — that’s roughly 14.97 orbits per day. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 years. As orbital debris, METEOR 2-5 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
METEOR 2-5 DEB orbits at an average altitude of 576 km in the core of Low Earth Orbit, the most heavily utilised altitude band. The balance of moderate drag (limiting debris accumulation) and short signal path (enabling low-latency links and high-resolution imaging) makes this regime the default for most commercial and government missions. Within ±50 km of METEOR 2-5 DEB’s average altitude, there are currently 3,070 active payloads and 511 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-2112, STARLINK-2722. This makes it one of the more crowded altitude bands, containing roughly 17.6% of all active satellites. With an inclination of 81.1°, METEOR 2-5 DEB passes over latitudes between 81.1°N and 81.1°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 1,285 active satellites in total, of which 32 share a similar altitude band with METEOR 2-5 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
METEOR 2-5 DEB orbits in Low Earth Orbit (LEO) at altitudes between 570 km (perigee) and 581 km (apogee), with an average altitude of approximately 576 km. It completes one orbit every 96 minutes, travelling at approximately 27,270 km/h (16,945 mph).
METEOR 2-5 DEB (NORAD ID 38275) 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.
METEOR 2-5 DEB was launched on 1979-10-31 from PKMTR. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks METEOR 2-5 DEB (NORAD ID 38275) 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.
METEOR 2-5 DEB travels at approximately 27,270 km/h (16,945 mph) — roughly 7.58 km/s. It completes 14.97 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 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 7.58 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 METEOR 2-5 DEB. Read more about debris statistics and the Kessler syndrome.