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: 8 hours ago
TLE from 8 hours ago
0 GONETS M 18
1 46487U 20068B 25311.88562817 .00000034 00000-0 17270-3 0 9999
2 46487 82.4891 124.3866 0020315 153.8215 206.3896 12.42890853231652Epoch: 2025-11-07T21:15Z
TLE epoch observation values (Epoch: 2025-11-07T21:15:18.273Z)
Latitude
-0.00005°
Longitude
118.23729°
Altitude
1,511.407 km
Speed
7.103 km/s
True Right ascension
08h 17m 32s
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
01:14:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,507.712 km
Perigee altitude
1,475.736 km
Semi-major axis
7,869.861 km
Eccentricity
0.00203
Inclination
82.4891°
RAAN
124.3866°
Arg. of periapsis
153.8215°
True anomaly
206.28636°
Mean anomaly
206.3896°
Eccentric anomaly
206.33796°
Mean motion
3.1088 °/min
Orbital period
115.8 mins
BSTAR
0.0001727
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-11-08 10:53:57.739Z | 128.596° SE | 2025-11-08 10:59:57.739Z | 79.972° E | 23.639° | 2025-11-08 11:05:57.739Z | 33.185° NE |
| 15 mins | 2025-11-08 12:48:57.739Z | 202.02° SSW | 2025-11-08 12:55:57.739Z | 284.485° WNW | 42.276° | 2025-11-08 13:03:57.739Z | 1.622° NNE |
| 4 mins | 2025-11-08 14:52:57.739Z | 291.189° WNW | 2025-11-08 14:54:57.739Z | 305.301° NW | 11.739° | 2025-11-08 14:56:57.739Z | 319.195° NNW |
| 15 mins | 2025-11-08 22:59:57.739Z | 1.656° NNE | 2025-11-08 23:06:57.739Z | 82.568° E | 41.462° | 2025-11-08 23:14:57.739Z | 158.216° S |
| 11 mins | 2025-11-09 00:57:57.739Z | 321.376° NNW | 2025-11-09 01:02:57.739Z | 277.855° WNW | 24.459° | 2025-11-09 01:08:57.739Z | 228.757° WSW |
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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