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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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Iframe URL

https://www.satcat.com/sats-embedded/57166?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

57166, 2023-091A

Orbit

SSO

Last TLE update

8 hours ago

Origin

Federal Service for Hydrometeorology and Environmental Monitoring (CIS)

Manufacturer

VNIIEM

Mission

Operational Civil Weather

Bus & Motor

RESURS-O, Unknown motor

Mass

2,879 kg wet, ~2,600 kg dry

Launch date (UTC)

2023-06-27 (2 years ago)

Launch vehicle

SOYUZ-2-1B

Launch site

Vostochny Cosmodrome (VOSTO)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl + 2 Pan, 7.0 m

Radar Cross Section

26.744 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 8 hours ago

0 METEOR M2-3
1 57166U 23091A   25201.03454252 -.00000020  00000-0  10417-4 0  9995
2 57166  98.6590 256.9284 0004958  64.3168 295.8522 14.24004089107243

Epoch: 2025-07-20T00:49Z

TLE epoch observation values (Epoch: 2025-07-20T00:49:44.473Z)

Latitude

-0.00008°

Longitude

-53.56998°

Altitude

813.211 km

Speed

7.447 km/s

True Right ascension

17h 07m 42s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

8.61078°

Longitude

-54.53675°

Altitude

811.988 km

Speed

7.449 km/s

Apparent Right ascension

14h 29m 48s

Apparent Declination

-21° 23' 18"

Sunlit

Object is in full shadow

Visualization observer readout

Local Sidereal Time

22:11:14

Azimuth

268.379° W

Elevation

-32.675°

Doppler factor

Orbital elements

Apogee altitude

812.557 km

Perigee altitude

805.43 km

Semi-major axis

7,187.131 km

Eccentricity

0.0005

Inclination

98.659°

RAAN

256.9284°

Arg. of periapsis

64.3168°

True anomaly

295.80106°

Mean anomaly

295.8522°

Eccentric anomaly

295.82663°

Mean motion

3.56213 °/min

Orbital period

101.06 mins

BSTAR

0.000010417

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Other satellites on launch #91 in the year 2023 (2023-06-27 UTC)

OBJECT AJ, 57198 (Decayed)

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.
9 mins	2025-07-20 16:35:04.561Z	16.217° NNE	2025-07-20 16:40:04.561Z	162.547° S	43.636°	2025-07-20 16:44:04.561Z	190.454° SSW
4 mins	2025-07-21 02:19:04.561Z	79.423° E	2025-07-21 02:20:04.561Z	66.669° ENE	14.958°	2025-07-21 02:23:04.561Z	30.008° NE
8 mins	2025-07-21 03:56:04.561Z	177.476° S	2025-07-21 04:00:04.561Z	279.593° WNW	42.712°	2025-07-21 04:04:04.561Z	339.59° N

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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Check out METEOR M2-3, 57166 on other resources

View METEOR M2-3, 57166 on NASA - NSSDCA Website

View METEOR M2-3, 57166 on Heavens-Above

View METEOR M2-3, 57166 on Keep Track

View METEOR M2-3, 57166 on Celestrak

View METEOR M2-3, 57166 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.