METEOR M2-4, 59051
Orbit data source: Space-Track
METEOR M2-4, 59051 is a Commonwealth of Independent States-origin payload satellite in SSO that was launched on Thu, 29 Feb 2024 UTC via a SOYUZ-2-1B launch vehicle from the Vostochny Cosmodrome (VOSTO). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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59051 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
VNIIEM
Mission
Operational Civil Weather
Bus & Motor
RESURS-O, Unknown motor
Mass
3,200 kg wet, ~3,000 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + 2 Pan, 7.0 m
Radar Cross Section
26.744 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 METEOR M2-4
1 59051U 24039A 25272.28136142 .00000114 00000-0 70630-4 0 9999
2 59051 98.6623 230.4058 0006555 196.6941 163.4022 14.22383267 82179Epoch: 2025-09-29T06:45Z
TLE epoch observation values (Epoch: 2025-09-29T06:45:09.626Z)
Latitude
-0.00005°
Longitude
120.82837°
Altitude
824.745 km
Speed
7.438 km/s
True Right ascension
15h 21m 37s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
12:09:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
819.172 km
Perigee altitude
809.742 km
Semi-major axis
7,192.594 km
Eccentricity
0.00066
Inclination
98.6623°
RAAN
230.4058°
Arg. of periapsis
196.6941°
True anomaly
163.42364°
Mean anomaly
163.4022°
Eccentric anomaly
163.41292°
Mean motion
3.55807 °/min
Orbital period
101.18 mins
BSTAR
0.00007063
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Other satellites on launch #39 in the year 2024 (2024-02-29 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.METEOR M2-4 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-09-29 20:24:10.444Z | 120.983° SE | 2025-09-29 20:28:10.444Z | 58.946° ENE | 27.03° | 2025-09-29 20:32:10.444Z | 8.389° NNE |
| 8 mins | 2025-09-29 22:04:10.444Z | 207.965° SW | 2025-09-29 22:08:10.444Z | 273.498° WNW | 27.986° | 2025-09-29 22:12:10.444Z | 324.841° NNW |
| 9 mins | 2025-09-30 10:21:10.444Z | 9.527° NNE | 2025-09-30 10:25:10.444Z | 266.158° W | 44.371° | 2025-09-30 10:30:10.444Z | 200° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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