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: 10 hours ago
TLE from 10 hours ago
0 GONETS M 17
1 46486U 20068A 25256.29507855 .00000035 00000-0 18076-3 0 9998
2 46486 82.5016 159.7562 0021864 281.8659 77.9969 12.42860884224768Epoch: 2025-09-13T07:04Z
TLE epoch observation values (Epoch: 2025-09-13T07:04:54.786Z)
Latitude
-0.00002°
Longitude
60.99743°
Altitude
1,493.654 km
Speed
7.119 km/s
True Right ascension
10h 39m 01s
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
09:53:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,509.057 km
Perigee altitude
1,474.643 km
Semi-major axis
7,869.987 km
Eccentricity
0.00219
Inclination
82.5016°
RAAN
159.7562°
Arg. of periapsis
281.8659°
True anomaly
78.2421°
Mean anomaly
77.9969°
Eccentric anomaly
78.11949°
Mean motion
3.10872 °/min
Orbital period
115.8 mins
BSTAR
0.00018076
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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. |
|---|---|---|---|---|---|---|---|
| 17 mins | 2025-09-13 18:44:58.050Z | 197.024° SSW | 2025-09-13 18:53:58.050Z | 296.011° NW | 42.855° | 2025-09-13 19:01:58.050Z | 2.861° NNE |
| 5 mins | 2025-09-13 20:49:58.050Z | 285.784° WNW | 2025-09-13 20:51:58.050Z | 300.003° NW | 12.659° | 2025-09-13 20:54:58.050Z | 321.23° NNW |
| 15 mins | 2025-09-14 04:57:58.050Z | 3.154° NNE | 2025-09-14 05:04:58.050Z | 84.173° E | 40.69° | 2025-09-14 05:12:58.050Z | 156.257° SSE |
| 13 mins | 2025-09-14 06:54:58.050Z | 326.997° NNW | 2025-09-14 07:00:58.050Z | 277.093° WNW | 25.94° | 2025-09-14 07:07:58.050Z | 222.643° SW |
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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