GONETS M 18, 46487
Orbit data source: Space-Track
GONETS M 18, 46487 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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46487 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: 22 hours ago
TLE from 22 hours ago
0 GONETS M 18
1 46487U 20068B 26172.51996069 .00000149 00000-0 10055-2 0 9995
2 46487 82.4948 343.9224 0020138 25.1407 335.0649 12.42874026259682Epoch: 2026-06-21T12:28Z
TLE epoch observation values (Epoch: 2026-06-21T12:28:44.603Z)
Latitude
0.00001°
Longitude
-112.9825°
Altitude
1,482.77 km
Speed
7.129 km/s
True Right ascension
22h 55m 41s
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
21:36:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,507.643 km
Perigee altitude
1,475.946 km
Semi-major axis
7,869.932 km
Eccentricity
0.00201
Inclination
82.4948°
RAAN
343.9224°
Arg. of periapsis
25.1407°
True anomaly
334.96739°
Mean anomaly
335.0649°
Eccentric anomaly
335.01617°
Mean motion
3.10876 °/min
Orbital period
115.8 mins
BSTAR
0.0010055
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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 18 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 | 2026-06-22 11:44:47.198Z | 171.426° S | 2026-06-22 11:52:47.198Z | 82.644° E | 42.554° | 2026-06-22 12:00:47.198Z | 13.359° NNE |
| 12 mins | 2026-06-22 13:44:47.198Z | 247.603° W | 2026-06-22 13:49:47.198Z | 290.004° WNW | 23.577° | 2026-06-22 13:56:47.198Z | 345.479° N |
| 13 mins | 2026-06-22 21:56:47.198Z | 15.474° NNE | 2026-06-22 22:02:47.198Z | 67.095° ENE | 27.792° | 2026-06-22 22:09:47.198Z | 127.014° SE |
| 14 mins | 2026-06-22 23:53:47.198Z | 339.559° N | 2026-06-22 23:59:47.198Z | 280.322° WNW | 39.354° | 2026-06-23 00:07:47.198Z | 196.96° SSW |
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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