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METEOR 2-6 DEB

NORAD 29199 Debris LEO 1980-073E
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🛰️ Orbital Parameters
Perigee
553 km
Apogee
567 km
Inclination
81.2°
Period
95.8 min
Mean Motion
15.02270151 rev/day
TLE Epoch
2026-11-08 02:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude560 km
Orbital Velocity27,301 km/h
Velocity7.58 km/s
Orbital Period96 minutes
Orbits / Day15.02
Eccentricity0.0010
Semi-Major Axis6,931 km
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1980-09-09
Launch Site
Plesetsk Cosmodrome, Russia
Int'l Designator
1980-073E
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
METEOR 2-6 DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 1980-09-09 from Plesetsk Cosmodrome, Russia on the Meteor-2 No. 5 launch. With over 46 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 553 km and 567 km with an inclination of 81.2°. It travels at approximately 27,301 km/h (7.58 km/s), completing one full orbit every 96 minutes — that’s roughly 15.02 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 years. As orbital debris, METEOR 2-6 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 2-6 DEB orbits at an average altitude of 560 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 2-6 DEB’s average altitude, there are currently 1,409 active payloads and 465 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 7.1% of all active satellites. With an inclination of 81.2°, METEOR 2-6 DEB passes over latitudes between 81.2°N and 81.2°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 1,575 active satellites in total, of which 39 share a similar altitude band with METEOR 2-6 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 2-6 DEB orbits in Low Earth Orbit (LEO) at altitudes between 553 km (perigee) and 567 km (apogee), with an average altitude of approximately 560 km. It completes one orbit every 96 minutes, travelling at approximately 27,301 km/h (16,964 mph).
METEOR 2-6 DEB (NORAD ID 29199) 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 2-6 DEB was launched on 1980-09-09 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 2-6 DEB (NORAD ID 29199) 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 2-6 DEB travels at approximately 27,301 km/h (16,964 mph) — roughly 7.58 km/s. It completes 15.02 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 2-6 DEB. Read more about debris statistics and the Kessler syndrome.