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METEOR 2-5 DEB

NORAD 38275 Debris LEO 1979-095BV
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🛰️ Orbital Parameters
Perigee
510 km
Apogee
538 km
Inclination
81.1°
Period
95.1 min
Mean Motion
15.14009175 rev/day
TLE Epoch
2026-11-01 13:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude524 km
Orbital Velocity27,372 km/h
Velocity7.60 km/s
Orbital Period95 minutes
Orbits / Day15.14
Eccentricity0.0020
Semi-Major Axis6,895 km
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1979-10-31
Launch Site
Plesetsk Cosmodrome, Russia
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 Plesetsk Cosmodrome, Russia 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 510 km and 538 km with an inclination of 81.1°. It travels at approximately 27,372 km/h (7.60 km/s), completing one full orbit every 95 minutes — that’s roughly 15.14 orbits per day. 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 524 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 5,076 active payloads and 294 tracked debris or rocket body fragments — notable neighbours include STARLINK-1184, STARLINK-1276, STARLINK-1451. This makes it one of the more crowded altitude bands, containing roughly 26.8% 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 1,550 active satellites in total, of which 74 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 510 km (perigee) and 538 km (apogee), with an average altitude of approximately 524 km. It completes one orbit every 95 minutes, travelling at approximately 27,372 km/h (17,008 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 Plesetsk Cosmodrome, Russia, Russia’s northern military cosmodrome, used primarily for high-inclination and polar orbit launches. 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) orbital data in its live tracking catalogue (see our data sources). 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 27,372 km/h (17,008 mph) — roughly 7.60 km/s. It completes 15.14 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 7.60 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.