GONETS-M 25, 54152
Orbit data source: Space-Track
GONETS-M 25, 54152 is a payload satellite owned by Gonets (CIS) in LEO that was launched on Sat, 22 Oct 2022 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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54152 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
Resehetnev ISS
Mission
Operational Commercial Communications
Bus & Motor
STRELA-3M, Unknown motor
Mass
280 kg wet, 280 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + 1 Ant, 3.5 m
Radar Cross Section
1.583 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 GONETS-M 25
1 54152U 22139C 25272.32843003 .00000035 00000-0 17959-3 0 9997
2 54152 82.5055 150.1896 0021125 78.2453 282.0995 12.42855050133244Epoch: 2025-09-29T07:52Z
TLE epoch observation values (Epoch: 2025-09-29T07:52:56.354Z)
Latitude
-0.00004°
Longitude
23.62106°
Altitude
1,493.77 km
Speed
7.119 km/s
True Right ascension
10h 00m 45s
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
12:32:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,508.5 km
Perigee altitude
1,475.249 km
Semi-major axis
7,870.012 km
Eccentricity
0.00211
Inclination
82.5055°
RAAN
150.1896°
Arg. of periapsis
78.2453°
True anomaly
281.86267°
Mean anomaly
282.0995°
Eccentric anomaly
281.9811°
Mean motion
3.10871 °/min
Orbital period
115.8 mins
BSTAR
0.00017959
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Other satellites on launch #139 in the year 2022 (2022-10-22 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.GONETS-M 25 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-09-30 01:53:33.766Z | 23.635° NE | 2025-09-30 01:58:33.766Z | 60.349° ENE | 17.351° | 2025-09-30 02:03:33.766Z | 98.451° ESE |
| 16 mins | 2025-09-30 03:49:33.766Z | 352.477° N | 2025-09-30 03:56:33.766Z | 357.444° N | 44.854° | 2025-09-30 04:05:33.766Z | 174.671° S |
| 8 mins | 2025-09-30 05:48:33.766Z | 311.898° NW | 2025-09-30 05:52:33.766Z | 281.68° WNW | 16.335° | 2025-09-30 05:56:33.766Z | 251.907° W |
| 10 mins | 2025-09-30 14:56:33.766Z | 113.515° SE | 2025-09-30 15:00:33.766Z | 81.526° E | 19.464° | 2025-09-30 15:06:33.766Z | 36.488° NE |
| 15 mins | 2025-09-30 16:49:33.766Z | 193.129° SSW | 2025-09-30 16:56:33.766Z | 277.393° WNW | 44.346° | 2025-09-30 17:04:33.766Z | 4.726° NNE |
| 6 mins | 2025-09-30 18:51:33.766Z | 274.712° WNW | 2025-09-30 18:54:33.766Z | 296.768° NW | 14.475° | 2025-09-30 18:57:33.766Z | 319.5° NNW |
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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