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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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: 1 day ago
TLE from 1 day ago
0 GONETS-M 23
1 54150U 22139A 26172.52910718 .00000039 00000-0 21093-3 0 9993
2 54150 82.5072 345.5955 0021060 209.8949 150.0930 12.42891026166182Epoch: 2026-06-21T12:41Z
TLE epoch observation values (Epoch: 2026-06-21T12:41:54.860Z)
Latitude
0.00005°
Longitude
-114.61115°
Altitude
1,511.454 km
Speed
7.103 km/s
True Right ascension
23h 02m 22s
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
00:51:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,508.296 km
Perigee altitude
1,475.149 km
Semi-major axis
7,869.86 km
Eccentricity
0.00211
Inclination
82.5072°
RAAN
345.5955°
Arg. of periapsis
209.8949°
True anomaly
150.21305°
Mean anomaly
150.093°
Eccentric anomaly
150.15305°
Mean motion
3.1088 °/min
Orbital period
115.8 mins
BSTAR
0.00021093
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-06-22 13:57:31.802Z | 247.026° WSW | 2026-06-22 14:03:31.802Z | 294.328° NW | 22.148° | 2026-06-22 14:09:31.802Z | 341.159° N |
| 13 mins | 2026-06-22 22:10:31.802Z | 15.554° NNE | 2026-06-22 22:16:31.802Z | 71.249° E | 29.648° | 2026-06-22 22:23:31.802Z | 131.599° SE |
| 15 mins | 2026-06-23 00:06:31.802Z | 339.416° N | 2026-06-23 00:13:31.802Z | 271.652° WNW | 37.634° | 2026-06-23 00:21:31.802Z | 199.629° SSW |
| 14 mins | 2026-06-23 11:10:31.802Z | 146.346° SSE | 2026-06-23 11:16:31.802Z | 90.802° ESE | 33.138° | 2026-06-23 11:24:31.802Z | 22.125° NNE |
| 15 mins | 2026-06-23 13:06:31.802Z | 220.252° SW | 2026-06-23 13:13:31.802Z | 286.375° WNW | 34.446° | 2026-06-23 13:21:31.802Z | 355.146° 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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