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METEOR 2-4

NORAD 11288 Payload LEO 1979-021A ● Active
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Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
834 km
Apogee
869 km
Inclination
81.2°
Period
102.0 min
Mean Motion
14.12326242 rev/day
TLE Epoch
2026-05-08 13:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude852 km
Orbital Velocity26,744 km/h
Velocity7.43 km/s
Orbital Period102 minutes
Orbits / Day14.12
Eccentricity0.0024
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 834 km and 869 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 occupies the mid-LEO band between 600 and 1,000 km, where atmospheric drag is minimal but radiation exposure remains low. This altitude range balances orbital longevity (decades to centuries) with reasonable ground coverage, making it popular for remote sensing constellations, scientific instruments and weather satellites. Debris concerns are significant here because objects persist far longer than in lower orbits.
❓ Frequently Asked Questions
METEOR 2-4 orbits in Low Earth Orbit (LEO) at altitudes between 834 km (perigee) and 869 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.
METEOR 2-4 was launched on 1979-03-01 from PKMTR. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years.
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.
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.
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