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 25342.79640713 .00000045 00000-0 24911-3 0 9997
2 46487 82.4926 105.1439 0020715 88.9737 271.3715 12.42892878235492Epoch: 2025-12-08T19:06Z
TLE epoch observation values (Epoch: 2025-12-08T19:06:49.576Z)
Latitude
-0.00009°
Longitude
100.64702°
Altitude
1,496.707 km
Speed
7.116 km/s
True Right ascension
07h 00m 34s
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
00:56:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,508.018 km
Perigee altitude
1,475.413 km
Semi-major axis
7,869.852 km
Eccentricity
0.00207
Inclination
82.4926°
RAAN
105.1439°
Arg. of periapsis
88.9737°
True anomaly
271.13418°
Mean anomaly
271.3715°
Eccentric anomaly
271.25284°
Mean motion
3.1088 °/min
Orbital period
115.8 mins
BSTAR
0.00024911
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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 | 2025-12-09 08:43:33.680Z | 173.03° S | 2025-12-09 08:51:33.680Z | 71.34° E | 42.959° | 2025-12-09 08:59:33.680Z | 12.398° NNE |
| 11 mins | 2025-12-09 10:43:33.680Z | 250.241° W | 2025-12-09 10:48:33.680Z | 292.437° WNW | 22.714° | 2025-12-09 10:54:33.680Z | 341.008° N |
| 13 mins | 2025-12-09 18:55:33.680Z | 16.139° NNE | 2025-12-09 19:01:33.680Z | 70.864° E | 28.593° | 2025-12-09 19:08:33.680Z | 129.915° SE |
| 15 mins | 2025-12-09 20:51:33.680Z | 340.441° N | 2025-12-09 20:58:33.680Z | 272.419° WNW | 38.554° | 2025-12-09 21:06:33.680Z | 197.931° SSW |
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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