Skip to content
Home Library Satellite Directory METEOR 2-1 DEB

METEOR 2-1 DEB

NORAD 57492 Debris LEO 1975-064F
CONNECTING… LEO · NORAD 57492
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
787 km
Apogee
800 km
Inclination
81.3°
Period
100.7 min
Mean Motion
14.29459636 rev/day
TLE Epoch
2026-06-14 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude794 km
Orbital Velocity26,852 km/h
Velocity7.46 km/s
Orbital Period101 minutes
Orbits / Day14.29
Eccentricity0.0009
Semi-Major Axis7,165 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1975-07-11
Launch Site
PKMTR
Int'l Designator
1975-064F
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
METEOR 2-1 DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 1975-07-11 from PKMTR on the Meteor-2 No. 1 launch. After more than 51 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Low Earth Orbit (LEO) at altitudes between 787 km and 800 km with an inclination of 81.3°. It travels at approximately 26,852 km/h (7.46 km/s), completing one full orbit every 101 minutes — that’s roughly 14.29 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 ~25–100 years. As orbital debris, METEOR 2-1 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 2-1 DEB orbits at an average altitude of 794 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of METEOR 2-1 DEB’s average altitude, there are currently 428 active payloads and 2,254 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 81.3°, METEOR 2-1 DEB passes over latitudes between 81.3°N and 81.3°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 66 share a similar altitude band with METEOR 2-1 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 2-1 DEB orbits in Low Earth Orbit (LEO) at altitudes between 787 km (perigee) and 800 km (apogee), with an average altitude of approximately 794 km. It completes one orbit every 101 minutes, travelling at approximately 26,852 km/h (16,685 mph).
METEOR 2-1 DEB (NORAD ID 57492) 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 2-1 DEB was launched on 1975-07-11 from PKMTR. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks METEOR 2-1 DEB (NORAD ID 57492) 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 2-1 DEB travels at approximately 26,852 km/h (16,685 mph) — roughly 7.46 km/s. It completes 14.29 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 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 7.46 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 2-1 DEB. Read more about debris statistics and the Kessler syndrome.