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: 8 hours ago
TLE from 8 hours ago
0 GONETS M 17
1 46486U 20068A 25312.48322127 .00000029 00000-0 13630-3 0 9993
2 46486 82.4938 124.8093 0022936 155.8793 204.3366 12.42864204231745Epoch: 2025-11-08T11:35Z
TLE epoch observation values (Epoch: 2025-11-08T11:35:50.317Z)
Latitude
-0.00003°
Longitude
-97.06254°
Altitude
1,513.646 km
Speed
7.101 km/s
True Right ascension
08h 19m 14s
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
16:15:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,509.887 km
Perigee altitude
1,473.786 km
Semi-major axis
7,869.973 km
Eccentricity
0.00229
Inclination
82.4938°
RAAN
124.8093°
Arg. of periapsis
155.8793°
True anomaly
204.22857°
Mean anomaly
204.3366°
Eccentric anomaly
204.28256°
Mean motion
3.10873 °/min
Orbital period
115.8 mins
BSTAR
0.0001363
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-11-08 21:52:52.947Z | 19.817° NNE | 2025-11-08 21:58:52.947Z | 67.872° E | 21.686° | 2025-11-08 22:04:52.947Z | 114.329° SE |
| 16 mins | 2025-11-08 23:48:52.947Z | 347.598° N | 2025-11-08 23:55:52.947Z | 291.177° WNW | 43.514° | 2025-11-09 00:04:52.947Z | 183.955° SSW |
| 4 mins | 2025-11-09 01:49:52.947Z | 297.388° NW | 2025-11-09 01:51:52.947Z | 283.07° WNW | 11.858° | 2025-11-09 01:53:52.947Z | 269.021° W |
| 11 mins | 2025-11-09 10:54:52.947Z | 125.821° SE | 2025-11-09 10:59:52.947Z | 82.59° E | 24.683° | 2025-11-09 11:05:52.947Z | 33.675° NE |
| 15 mins | 2025-11-09 12:48:52.947Z | 203.576° SW | 2025-11-09 12:55:52.947Z | 275.993° WNW | 41.563° | 2025-11-09 13:03:52.947Z | 0.337° 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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