Skip to content
Home Library Satellite Directory METEOR 2-10

METEOR 2-10

NORAD 14452 Payload LEO 1983-109A ● Active
CONNECTING… LEO · NORAD 14452
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
736 km
Apogee
865 km
Inclination
81.2°
Period
100.9 min
Mean Motion
14.27277097 rev/day
TLE Epoch
2026-06-19 14:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude801 km
Orbital Velocity26,839 km/h
Velocity7.46 km/s
Orbital Period101 minutes
Orbits / Day14.27
Eccentricity0.0090
Semi-Major Axis7,172 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1983-10-28
Launch Site
PKMTR
Int'l Designator
1983-109A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
METEOR 2-10 is an active satellite operated by Russia (CIS), launched on 1983-10-28 from PKMTR. With over 43 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 736 km and 865 km with an inclination of 81.2°. It travels at approximately 26,839 km/h (7.46 km/s), completing one full orbit every 101 minutes — that’s roughly 14.27 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Orbital Radar tracks METEOR 2-10 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
METEOR 2-10 orbits at an average altitude of 801 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 METEOR 2-10’s average altitude, there are currently 444 active payloads and 2,272 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 81.2°, METEOR 2-10 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 1,286 active satellites in total, of which 79 share a similar altitude band with METEOR 2-10.
❓ Frequently Asked Questions
METEOR 2-10 orbits in Low Earth Orbit (LEO) at altitudes between 736 km (perigee) and 865 km (apogee), with an average altitude of approximately 801 km. It completes one orbit every 101 minutes, travelling at approximately 26,839 km/h (16,677 mph).
METEOR 2-10 is operated by Russia (CIS). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 14452. You can track METEOR 2-10 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
METEOR 2-10 was launched on 1983-10-28 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 METEOR 2-10 (NORAD ID 14452) 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 2-10 travels at approximately 26,839 km/h (16,677 mph) — roughly 7.46 km/s. It completes 14.27 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.