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METEOR 2-4

NORAD 11288 Payload LEO 1979-021A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
835 km
Apogee
868 km
Inclination
81.2°
Period
102.0 min
Mean Motion
14.12332811 rev/day
TLE Epoch
2026-06-19 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude852 km
Orbital Velocity26,744 km/h
Velocity7.43 km/s
Orbital Period102 minutes
Orbits / Day14.12
Eccentricity0.0023
Semi-Major Axis7,223 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1979-03-01
Launch Site
PKMTR
Int'l Designator
1979-021A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
METEOR 2-4 is an active satellite operated by Russia (CIS), launched on 1979-03-01 from PKMTR. With over 47 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 835 km and 868 km with an inclination of 81.2°. It travels at approximately 26,744 km/h (7.43 km/s), completing one full orbit every 102 minutes — that’s roughly 14.12 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Orbital Radar tracks METEOR 2-4 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 2-4 orbits at an average altitude of 852 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 2-4’s average altitude, there are currently 267 active payloads and 2,020 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 81.2°, METEOR 2-4 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 1,285 active satellites in total, of which 48 share a similar altitude band with METEOR 2-4.
❓ Frequently Asked Questions
METEOR 2-4 orbits in Low Earth Orbit (LEO) at altitudes between 835 km (perigee) and 868 km (apogee), with an average altitude of approximately 852 km. It completes one orbit every 102 minutes, travelling at approximately 26,744 km/h (16,618 mph).
METEOR 2-4 is operated by Russia (CIS). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 11288. You can track METEOR 2-4 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
METEOR 2-4 was launched on 1979-03-01 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 2-4 (NORAD ID 11288) 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 2-4 travels at approximately 26,744 km/h (16,618 mph) — roughly 7.43 km/s. It completes 14.12 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.