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: 10 hours ago
TLE from 10 hours ago
0 GONETS M 17
1 46486U 20068A 26304.89405931 .00000039 00000-0 20522-3 0 9994
2 46486 82.4958 262.4443 0023709 95.9973 264.3809 12.42888214276146Epoch: 2026-10-31T21:27Z
TLE epoch observation values (Epoch: 2026-10-31T21:27:26.724Z)
Latitude
-0.00007°
Longitude
-99.6103°
Altitude
1,498.955 km
Speed
7.114 km/s
True Right ascension
17h 29m 46s
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
03:25:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,510.394 km
Perigee altitude
1,473.076 km
Semi-major axis
7,869.872 km
Eccentricity
0.00237
Inclination
82.4958°
RAAN
262.4443°
Arg. of periapsis
95.9973°
True anomaly
264.1106°
Mean anomaly
264.3809°
Eccentric anomaly
264.24574°
Mean motion
3.10879 °/min
Orbital period
115.8 mins
BSTAR
0.00020522
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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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2026-11-01 07:43:44.037Z | 14.459° NNE | 2026-11-01 07:50:44.037Z | 71.146° E | 27.112° | 2026-11-01 07:56:44.037Z | 119.557° SE |
| 15 mins | 2026-11-01 09:40:44.037Z | 344.367° N | 2026-11-01 09:47:44.037Z | 272.79° WNW | 64.156° | 2026-11-01 09:55:44.037Z | 190.244° SSW |
| 12 mins | 2026-11-01 20:45:44.037Z | 134.102° SE | 2026-11-01 20:51:44.037Z | 79.061° E | 31.4° | 2026-11-01 20:57:44.037Z | 29.962° NE |
| 15 mins | 2026-11-01 22:40:44.037Z | 210.227° SW | 2026-11-01 22:47:44.037Z | 284.389° WNW | 54.333° | 2026-11-01 22:55:44.037Z | 358.623° N |
| 6 mins | 2026-11-02 06:57:44.037Z | 41.677° NE | 2026-11-02 06:59:44.037Z | 56.398° ENE | 14.079° | 2026-11-02 07:03:44.037Z | 85.3° E |
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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