GONETS M 17, 46486
Orbit data source: Space-Track
GONETS M 17, 46486 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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46486 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: 5 hours ago
TLE from 5 hours ago
0 GONETS M 17
1 46486U 20068A 25342.58969351 .00000038 00000-0 20312-3 0 9998
2 46486 82.4966 106.0793 0023314 92.5318 267.8431 12.42865689235486Epoch: 2025-12-08T14:09Z
TLE epoch observation values (Epoch: 2025-12-08T14:09:09.519Z)
Latitude
-0.00001°
Longitude
176.20308°
Altitude
1,497.912 km
Speed
7.115 km/s
True Right ascension
07h 04m 19s
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
17:40:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,510.178 km
Perigee altitude
1,473.482 km
Semi-major axis
7,869.967 km
Eccentricity
0.00233
Inclination
82.4966°
RAAN
106.0793°
Arg. of periapsis
92.5318°
True anomaly
267.57616°
Mean anomaly
267.8431°
Eccentric anomaly
267.70963°
Mean motion
3.10874 °/min
Orbital period
115.8 mins
BSTAR
0.00020312
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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 17 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 | 2025-12-08 20:34:02.423Z | 348.48° N | 2025-12-08 20:42:02.423Z | 249.51° W | 44.031° | 2025-12-08 20:50:02.423Z | 182.794° SSW |
| 5 mins | 2025-12-08 22:35:02.423Z | 299.334° NW | 2025-12-08 22:37:02.423Z | 284.888° WNW | 12.556° | 2025-12-08 22:40:02.423Z | 263.764° W |
| 12 mins | 2025-12-09 07:40:02.423Z | 126.889° SE | 2025-12-09 07:45:02.423Z | 86.002° E | 23.664° | 2025-12-09 07:52:02.423Z | 30.929° NE |
| 16 mins | 2025-12-09 09:34:02.423Z | 201.448° SSW | 2025-12-09 09:41:02.423Z | 264.574° W | 41.813° | 2025-12-09 09:50:02.423Z | 2.135° NNE |
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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