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: 9 hours ago
TLE from 9 hours ago
0 GONETS M 17
1 46486U 20068A 26307.63095707 .00000022 00000-0 86402-4 0 9997
2 46486 82.4956 260.7415 0023737 90.2393 270.1407 12.42888397276487Epoch: 2026-11-03T15:08Z
TLE epoch observation values (Epoch: 2026-11-03T15:08:34.690Z)
Latitude
-0.00001°
Longitude
-9.2939°
Altitude
1,497.081 km
Speed
7.116 km/s
True Right ascension
17h 22m 57s
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
19:48:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,510.415 km
Perigee altitude
1,473.053 km
Semi-major axis
7,869.871 km
Eccentricity
0.00237
Inclination
82.4956°
RAAN
260.7415°
Arg. of periapsis
90.2393°
True anomaly
269.86869°
Mean anomaly
270.1407°
Eccentric anomaly
270.0047°
Mean motion
3.10879 °/min
Orbital period
115.8 mins
BSTAR
0.000086402
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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 | 2026-11-04 07:12:43.478Z | 17.61° NNE | 2026-11-04 07:18:43.478Z | 63.082° ENE | 22.865° | 2026-11-04 07:24:43.478Z | 110.916° ESE |
| 15 mins | 2026-11-04 09:09:43.478Z | 347.746° N | 2026-11-04 09:16:43.478Z | 264.973° W | 75.287° | 2026-11-04 09:24:43.478Z | 183.286° SSW |
| 5 mins | 2026-11-04 11:09:43.478Z | 300.937° NW | 2026-11-04 11:11:43.478Z | 286.657° WNW | 12.778° | 2026-11-04 11:14:43.478Z | 265.446° W |
| 12 mins | 2026-11-04 20:14:43.478Z | 128.099° SE | 2026-11-04 20:20:43.478Z | 77.455° E | 26.256° | 2026-11-04 20:26:43.478Z | 31.658° NE |
| 15 mins | 2026-11-04 22:09:43.478Z | 203.475° SW | 2026-11-04 22:16:43.478Z | 292.189° WNW | 63.415° | 2026-11-04 22:24:43.478Z | 1.678° 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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