METEOR M2-3, 57166
Orbit data source: Space-Track
METEOR M2-3, 57166 is a Commonwealth of Independent States-origin payload satellite in SSO that was launched on Tue, 27 Jun 2023 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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57166 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
2,879 kg wet, ~2,600 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: 7 hours ago
TLE from 7 hours ago
0 METEOR M2-3
1 57166U 23091A 25304.67397441 .00000027 00000-0 30689-4 0 9994
2 57166 98.6441 358.9348 0005037 110.4093 249.7627 14.24018212121996Epoch: 2025-10-31T16:10Z
TLE epoch observation values (Epoch: 2025-10-31T16:10:31.389Z)
Latitude
-0.00002°
Longitude
76.08899°
Altitude
815.972 km
Speed
7.445 km/s
True Right ascension
23h 55m 44s
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
18:24:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
812.566 km
Perigee altitude
805.325 km
Semi-major axis
7,187.083 km
Eccentricity
0.0005
Inclination
98.6441°
RAAN
358.9348°
Arg. of periapsis
110.4093°
True anomaly
249.70856°
Mean anomaly
249.7627°
Eccentric anomaly
249.73563°
Mean motion
3.56217 °/min
Orbital period
101.06 mins
BSTAR
0.000030689
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Other satellites on launch #91 in the year 2023 (2023-06-27 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 M2-3 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-01 02:27:42.500Z | 98.234° ESE | 2025-11-01 02:30:42.500Z | 58.112° ENE | 18.181° | 2025-11-01 02:33:42.500Z | 21.764° NNE |
| 9 mins | 2025-11-01 04:05:42.500Z | 185.25° SSW | 2025-11-01 04:09:42.500Z | 253.113° W | 39.111° | 2025-11-01 04:14:42.500Z | 336.327° NNW |
| 8 mins | 2025-11-01 16:22:42.500Z | 24.952° NE | 2025-11-01 16:26:42.500Z | 118.652° SE | 41.053° | 2025-11-01 16:30:42.500Z | 179.855° S |
| 5 mins | 2025-11-01 18:03:42.500Z | 325.212° NNW | 2025-11-01 18:05:42.500Z | 299.229° NW | 16.52° | 2025-11-01 18:08:42.500Z | 262.175° W |
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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