GONETS-M 24, 54151
Orbit data source: Space-Track
GONETS-M 24, 54151 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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54151 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: 7 hours ago
TLE from 7 hours ago
0 GONETS-M 24
1 54151U 22139B 25272.82510366 .00001143 00000-0 81805-2 0 9995
2 54151 82.4989 149.3346 0017222 78.2085 282.0926 12.42856049133302Epoch: 2025-09-29T19:48Z
TLE epoch observation values (Epoch: 2025-09-29T19:48:08.956Z)
Latitude
0.00005°
Longitude
-156.52598°
Altitude
1,494.4 km
Speed
7.118 km/s
True Right ascension
09h 57m 20s
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
20:33:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,505.424 km
Perigee altitude
1,478.317 km
Semi-major axis
7,870.008 km
Eccentricity
0.00172
Inclination
82.4989°
RAAN
149.3346°
Arg. of periapsis
78.2085°
True anomaly
281.89954°
Mean anomaly
282.0926°
Eccentric anomaly
281.99608°
Mean motion
3.10871 °/min
Orbital period
115.8 mins
BSTAR
0.0081805
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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 24 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. |
|---|---|---|---|---|---|---|---|
| 16 mins | 2025-09-30 04:09:01.953Z | 346.537° N | 2025-09-30 04:17:01.953Z | 255.285° W | 42.922° | 2025-09-30 04:25:01.953Z | 186.87° SSW |
| 12 mins | 2025-09-30 15:15:01.953Z | 129.656° SE | 2025-09-30 15:20:01.953Z | 85.97° E | 25.932° | 2025-09-30 15:27:01.953Z | 29.315° NE |
| 16 mins | 2025-09-30 17:09:01.953Z | 205.739° SW | 2025-09-30 17:16:01.953Z | 268.84° W | 40.172° | 2025-09-30 17:25:01.953Z | 0.641° NNE |
| 5 mins | 2025-10-01 01:27:01.953Z | 45.034° ENE | 2025-10-01 01:29:01.953Z | 59.533° ENE | 12.62° | 2025-10-01 01:32:01.953Z | 80.658° E |
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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