GONETS-M 23, 54150
Orbit data source: Space-Track
GONETS-M 23, 54150 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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54150 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: 14 hours ago
TLE from 14 hours ago
0 GONETS-M 23
1 54150U 22139A 25272.28911873 .00000023 00000-0 93540-4 0 9999
2 54150 82.5074 150.4300 0022063 69.9370 290.4081 12.42857458133235Epoch: 2025-09-29T06:56Z
TLE epoch observation values (Epoch: 2025-09-29T06:56:19.858Z)
Latitude
-0.0001°
Longitude
38.05227°
Altitude
1,491.189 km
Speed
7.121 km/s
True Right ascension
10h 01m 43s
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
14:21:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,509.228 km
Perigee altitude
1,474.501 km
Semi-major axis
7,870.001 km
Eccentricity
0.00221
Inclination
82.5074°
RAAN
150.43°
Arg. of periapsis
69.937°
True anomaly
290.17092°
Mean anomaly
290.4081°
Eccentric anomaly
290.28953°
Mean motion
3.10872 °/min
Orbital period
115.8 mins
BSTAR
0.00009354
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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 23 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. |
|---|---|---|---|---|---|---|---|
| 15 mins | 2025-09-30 02:52:28.633Z | 8.034° NNE | 2025-09-30 02:59:28.633Z | 72.056° E | 33.818° | 2025-09-30 03:07:28.633Z | 142.123° SSE |
| 14 mins | 2025-09-30 04:49:28.633Z | 335.49° NNW | 2025-09-30 04:56:28.633Z | 270.594° WNW | 33.432° | 2025-09-30 05:03:28.633Z | 209.433° SW |
| 14 mins | 2025-09-30 15:53:28.633Z | 154.866° SSE | 2025-09-30 15:59:28.633Z | 94.093° ESE | 37.154° | 2025-09-30 16:07:28.633Z | 19.059° NNE |
| 13 mins | 2025-09-30 17:50:28.633Z | 230.911° WSW | 2025-09-30 17:56:28.633Z | 284.973° WNW | 29.888° | 2025-09-30 18:03:28.633Z | 348.219° 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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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