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: 19 hours ago
TLE from 19 hours ago
0 GONETS M 17
1 46486U 20068A 25339.28925597 .00000015 00000-0 35467-4 0 9998
2 46486 82.4963 108.1322 0023332 99.4355 260.9364 12.42865554235076Epoch: 2025-12-05T06:56Z
TLE epoch observation values (Epoch: 2025-12-05T06:56:31.715Z)
Latitude
0.00001°
Longitude
-70.33343°
Altitude
1,500.115 km
Speed
7.113 km/s
True Right ascension
07h 12m 31s
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
23:55:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,510.193 km
Perigee altitude
1,473.468 km
Semi-major axis
7,869.968 km
Eccentricity
0.00233
Inclination
82.4963°
RAAN
108.1322°
Arg. of periapsis
99.4355°
True anomaly
260.6725°
Mean anomaly
260.9364°
Eccentric anomaly
260.80444°
Mean motion
3.10874 °/min
Orbital period
115.8 mins
BSTAR
0.000035467
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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. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2025-12-06 08:09:15.335Z | 140.686° SSE | 2025-12-06 08:16:15.335Z | 85.447° E | 27.356° | 2025-12-06 08:23:15.335Z | 28.127° NE |
| 15 mins | 2025-12-06 10:05:15.335Z | 208.427° SW | 2025-12-06 10:12:15.335Z | 271.687° WNW | 39.075° | 2025-12-06 10:20:15.335Z | 357.53° N |
| 6 mins | 2025-12-06 18:22:15.335Z | 38.26° NE | 2025-12-06 18:25:15.335Z | 60.21° ENE | 13.517° | 2025-12-06 18:28:15.335Z | 81.959° E |
| 16 mins | 2025-12-06 20:16:15.335Z | 357.12° N | 2025-12-06 20:23:15.335Z | 61.249° ENE | 43.659° | 2025-12-06 20:32:15.335Z | 165.875° S |
| 10 mins | 2025-12-06 22:15:15.335Z | 315.06° NNW | 2025-12-06 22:19:15.335Z | 282.069° WNW | 20.714° | 2025-12-06 22:25:15.335Z | 235.746° WSW |
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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