METEOR M2-4
NORAD 59051
Payload
LEO
2024-039A
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LEO · NORAD 59051
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
812 km
Apogee
822 km
Inclination
98.7°
Period
101.2 min
Mean Motion
14.22429704 rev/day
TLE Epoch
2026-06-19 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude817 km
Orbital Velocity26,808 km/h
Velocity7.45 km/s
Orbital Period101 minutes
Orbits / Day14.22
Eccentricity0.0007
Semi-Major Axis7,188 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2024-02-29
Launch Site
Vostochny, Russia
Int'l Designator
2024-039A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
METEOR M2-4 is an active satellite operated by Russia (CIS), launched on 2024-02-29 from Vostochny, Russia. It orbits in Low Earth Orbit (LEO) at altitudes between 812 km and 822 km with an inclination of 98.7°. It travels at approximately 26,808 km/h (7.45 km/s), completing one full orbit every 101 minutes — that’s roughly 14.22 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. 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 ~100–500 years. Orbital Radar tracks METEOR M2-4 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 M2-4 orbits at an average altitude of 817 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of METEOR M2-4’s average altitude, there are currently 409 active payloads and 2,290 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 98.7°, METEOR M2-4 passes over latitudes between 98.7°N and 98.7°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 81 share a similar altitude band with METEOR M2-4.
❓ Frequently Asked Questions
METEOR M2-4 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 817 km altitude. Its 98.7° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 101 minutes, travelling at 26,808 km/h.
METEOR M2-4 is operated by Russia (CIS). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 59051. You can track METEOR M2-4 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
METEOR M2-4 was launched on 2024-02-29 from Vostochny, Russia. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks METEOR M2-4 (NORAD ID 59051) 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 M2-4 travels at approximately 26,808 km/h (16,658 mph) — roughly 7.45 km/s. It completes 14.22 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.