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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METEOR M2-3 radio frequencies
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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: 12 hours ago
TLE from 12 hours ago
0 METEOR M2-3
1 57166U 23091A 25247.26837475 .00000041 00000-0 36957-4 0 9991
2 57166 98.6535 302.4595 0002840 285.2858 74.8007 14.24008977113826Epoch: 2025-09-04T06:26Z
TLE epoch observation values (Epoch: 2025-09-04T06:26:27.578Z)
Latitude
-0°
Longitude
-137.78875°
Altitude
814.213 km
Speed
7.446 km/s
True Right ascension
20h 09m 50s
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
10:46:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
811.018 km
Perigee altitude
806.936 km
Semi-major axis
7,187.114 km
Eccentricity
0.00028
Inclination
98.6535°
RAAN
302.4595°
Arg. of periapsis
285.2858°
True anomaly
74.83211°
Mean anomaly
74.8007°
Eccentric anomaly
74.8164°
Mean motion
3.56214 °/min
Orbital period
101.06 mins
BSTAR
0.000036957
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Other satellites on launch #91 in the year 2023 (2023-06-27 UTC)
METEOR M2-3 Visibility forecast
Observer location: undefined°, undefined°
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 | 2025-09-05 02:48:57.604Z | 122.197° SE | 2025-09-05 02:52:57.604Z | 65.481° ENE | 26.351° | 2025-09-05 02:56:57.604Z | 10.833° NNE |
| 8 mins | 2025-09-05 04:28:57.604Z | 205.156° SW | 2025-09-05 04:32:57.604Z | 269.474° W | 28.853° | 2025-09-05 04:36:57.604Z | 324.506° NNW |
| 9 mins | 2025-09-05 16:44:57.604Z | 11.304° NNE | 2025-09-05 16:48:57.604Z | 332.743° NNW | 44.525° | 2025-09-05 16:53:57.604Z | 198.236° 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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Authenticating...
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