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: 7 hours ago
TLE from 7 hours ago
0 GONETS M 17
1 46486U 20068A 25259.59552679 .00000020 00000-0 75834-4 0 9998
2 46486 82.5011 157.7046 0021810 274.3189 85.5398 12.42861004225176Epoch: 2025-09-16T14:17Z
TLE epoch observation values (Epoch: 2025-09-16T14:17:33.514Z)
Latitude
-0.00008°
Longitude
-52.46862°
Altitude
1,495.9 km
Speed
7.117 km/s
True Right ascension
10h 30m 49s
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
14:03:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,509.014 km
Perigee altitude
1,474.685 km
Semi-major axis
7,869.987 km
Eccentricity
0.00218
Inclination
82.5011°
RAAN
157.7046°
Arg. of periapsis
274.3189°
True anomaly
85.78902°
Mean anomaly
85.5398°
Eccentric anomaly
85.6644°
Mean motion
3.10872 °/min
Orbital period
115.8 mins
BSTAR
0.000075834
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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 | 2025-09-17 04:25:36.954Z | 2.927° NNE | 2025-09-17 04:33:36.954Z | 77.199° E | 37.704° | 2025-09-17 04:41:36.954Z | 149.454° SSE |
| 13 mins | 2025-09-17 06:23:36.954Z | 330.956° NNW | 2025-09-17 06:29:36.954Z | 280.487° WNW | 29.474° | 2025-09-17 06:36:36.954Z | 218.489° SW |
| 15 mins | 2025-09-17 17:26:36.954Z | 163.824° S | 2025-09-17 17:33:36.954Z | 80.895° E | 40.626° | 2025-09-17 17:41:36.954Z | 15.259° NNE |
| 13 mins | 2025-09-17 19:24:36.954Z | 239.41° WSW | 2025-09-17 19:30:36.954Z | 291.541° WNW | 26.474° | 2025-09-17 19:37:36.954Z | 347.581° 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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