GONETS M 18, 46487
Orbit data source: Space-Track
GONETS M 18, 46487 is a payload satellite owned by Gonets (CIS) in LEO that was launched on Mon, 28 Sep 2020 UTC via a SOYUZ-2-1B launch vehicle from the Plesetsk Missile And Space Complex (PKMTR). 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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46487 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
225 kg wet, 225 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + 1 Ant, 3.5 m
Radar Cross Section
1.798 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 GONETS M 18
1 46487U 20068B 25288.62198631 .00000034 00000-0 17752-3 0 9998
2 46487 82.4910 138.8703 0019490 204.6704 155.3445 12.42888834228761Epoch: 2025-10-15T14:55Z
TLE epoch observation values (Epoch: 2025-10-15T14:55:39.617Z)
Latitude
-0.00002°
Longitude
-109.4382°
Altitude
1,511.033 km
Speed
7.103 km/s
True Right ascension
09h 15m 28s
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
19:11:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,507.071 km
Perigee altitude
1,476.394 km
Semi-major axis
7,869.869 km
Eccentricity
0.00195
Inclination
82.491°
RAAN
138.8703°
Arg. of periapsis
204.6704°
True anomaly
155.43746°
Mean anomaly
155.3445°
Eccentric anomaly
155.391°
Mean motion
3.10879 °/min
Orbital period
115.8 mins
BSTAR
0.00017752
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Other satellites on launch #68 in the year 2020 (2020-09-28 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 18 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 | 2025-10-16 01:11:37.988Z | 3.466° NNE | 2025-10-16 01:19:37.988Z | 74.115° E | 36.175° | 2025-10-16 01:27:37.988Z | 146.541° SSE |
| 14 mins | 2025-10-16 03:09:37.988Z | 332.917° NNW | 2025-10-16 03:16:37.988Z | 269.078° W | 30.836° | 2025-10-16 03:23:37.988Z | 212.801° SW |
| 15 mins | 2025-10-16 14:12:37.988Z | 161.333° S | 2025-10-16 14:19:37.988Z | 87.409° E | 39.509° | 2025-10-16 14:27:37.988Z | 16.752° NNE |
| 13 mins | 2025-10-16 16:10:37.988Z | 236.185° WSW | 2025-10-16 16:16:37.988Z | 289.032° WNW | 27.954° | 2025-10-16 16:23:37.988Z | 347.646° N |
| 8 mins | 2025-10-17 00:24:37.988Z | 23.183° NE | 2025-10-17 00:29:37.988Z | 65.881° ENE | 23.683° | 2025-10-17 00:32:37.988Z | 95.157° ESE |
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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