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 25286.64311766 .00000036 00000-0 19023-3 0 9998
2 46486 82.4961 140.8861 0022033 212.6048 147.3673 12.42862631228537Epoch: 2025-10-13T15:26Z
TLE epoch observation values (Epoch: 2025-10-13T15:26:05.365Z)
Latitude
0.00002°
Longitude
-113.07921°
Altitude
1,511.812 km
Speed
7.102 km/s
True Right ascension
09h 23m 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
14:49:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,509.183 km
Perigee altitude
1,474.503 km
Semi-major axis
7,869.98 km
Eccentricity
0.0022
Inclination
82.4961°
RAAN
140.8861°
Arg. of periapsis
212.6048°
True anomaly
147.50313°
Mean anomaly
147.3673°
Eccentric anomaly
147.43525°
Mean motion
3.10873 °/min
Orbital period
115.8 mins
BSTAR
0.00019023
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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 | 2025-10-14 01:41:59.291Z | 359.898° N | 2025-10-14 01:49:59.291Z | 67.545° E | 39.962° | 2025-10-14 01:57:59.291Z | 153.777° SSE |
| 12 mins | 2025-10-14 03:40:59.291Z | 325.764° NNW | 2025-10-14 03:46:59.291Z | 272.711° WNW | 26.358° | 2025-10-14 03:52:59.291Z | 224.194° SW |
| 15 mins | 2025-10-14 14:42:59.291Z | 170.552° S | 2025-10-14 14:49:59.291Z | 93.204° ESE | 42.793° | 2025-10-14 14:57:59.291Z | 13.581° NNE |
| 12 mins | 2025-10-14 16:41:59.291Z | 246.389° WSW | 2025-10-14 16:47:59.291Z | 297.388° NW | 23.746° | 2025-10-14 16:53:59.291Z | 343.757° N |
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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