Skip to content
Home Library Satellite Directory METEOR 2-3

METEOR 2-3

NORAD 10514 Payload LEO 1977-117A ● Active
CONNECTING… LEO · NORAD 10514
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
839 km
Apogee
872 km
Inclination
81.2°
Period
102.0 min
Mean Motion
14.11240134 rev/day
TLE Epoch
2026-06-19 16:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude856 km
Orbital Velocity26,737 km/h
Velocity7.43 km/s
Orbital Period102 minutes
Orbits / Day14.11
Eccentricity0.0023
Semi-Major Axis7,227 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1977-12-14
Launch Site
PKMTR
Int'l Designator
1977-117A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
METEOR 2-3 is an active satellite operated by Russia (CIS), launched on 1977-12-14 from PKMTR. With over 49 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 839 km and 872 km with an inclination of 81.2°. It travels at approximately 26,737 km/h (7.43 km/s), completing one full orbit every 102 minutes — that’s roughly 14.11 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Orbital Radar tracks METEOR 2-3 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 2-3 orbits at an average altitude of 856 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 2-3’s average altitude, there are currently 260 active payloads and 1,974 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 81.2°, METEOR 2-3 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 57 share a similar altitude band with METEOR 2-3.
❓ Frequently Asked Questions
METEOR 2-3 orbits in Low Earth Orbit (LEO) at altitudes between 839 km (perigee) and 872 km (apogee), with an average altitude of approximately 856 km. It completes one orbit every 102 minutes, travelling at approximately 26,737 km/h (16,613 mph).
METEOR 2-3 is operated by Russia (CIS). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 10514. You can track METEOR 2-3 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
METEOR 2-3 was launched on 1977-12-14 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 2-3 (NORAD ID 10514) 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 2-3 travels at approximately 26,737 km/h (16,613 mph) — roughly 7.43 km/s. It completes 14.11 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.