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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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: 4 hours ago
TLE from 4 hours ago
0 GONETS M 17
1 46486U 20068A 26252.32941082 .00000039 00000-0 20779-3 0 9990
2 46486 82.4974 295.1647 0022049 208.8225 151.1638 12.42886556269618Epoch: 2026-09-09T07:54Z
TLE epoch observation values (Epoch: 2026-09-09T07:54:21.094Z)
Latitude
-0.00005°
Longitude
-171.80623°
Altitude
1,512.307 km
Speed
7.102 km/s
True Right ascension
19h 40m 39s
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
04:15:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,509.094 km
Perigee altitude
1,474.389 km
Semi-major axis
7,869.879 km
Eccentricity
0.0022
Inclination
82.4974°
RAAN
295.1647°
Arg. of periapsis
208.8225°
True anomaly
151.28537°
Mean anomaly
151.1638°
Eccentric anomaly
151.22461°
Mean motion
3.10879 °/min
Orbital period
115.8 mins
BSTAR
0.00020779
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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. |
|---|---|---|---|---|---|---|---|
| 15 mins | 2026-09-09 14:19:32.731Z | 1.889° NNE | 2026-09-09 14:26:32.731Z | 69.862° E | 58.68° | 2026-09-09 14:34:32.731Z | 155.111° SSE |
| 12 mins | 2026-09-09 16:17:32.731Z | 324.703° NNW | 2026-09-09 16:22:32.731Z | 282.829° WNW | 28.819° | 2026-09-09 16:29:32.731Z | 224.557° SW |
| 15 mins | 2026-09-10 03:19:32.731Z | 171.565° S | 2026-09-10 03:26:32.731Z | 86.092° E | 69.546° | 2026-09-10 03:34:32.731Z | 12.9° NNE |
| 12 mins | 2026-09-10 05:18:32.731Z | 248.112° W | 2026-09-10 05:23:32.731Z | 288.868° WNW | 25.442° | 2026-09-10 05:30:32.731Z | 344.135° 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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