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: 6 hours ago
TLE from 6 hours ago
0 GONETS M 18
1 46487U 20068B 26126.87760716 -.00000022 00000-0 -22862-3 0 9993
2 46487 82.4974 12.3360 0020406 119.5284 240.7834 12.42870370254016Epoch: 2026-05-06T21:03Z
TLE epoch observation values (Epoch: 2026-05-06T21:03:45.258Z)
Latitude
0.00002°
Longitude
-168.33436°
Altitude
1,505.026 km
Speed
7.109 km/s
True Right ascension
00h 49m 20s
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
11:32:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,507.87 km
Perigee altitude
1,475.751 km
Semi-major axis
7,869.947 km
Eccentricity
0.00204
Inclination
82.4974°
RAAN
12.336°
Arg. of periapsis
119.5284°
True anomaly
240.57957°
Mean anomaly
240.7834°
Eccentric anomaly
240.68146°
Mean motion
3.10875 °/min
Orbital period
115.8 mins
BSTAR
-0.00022862
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-05-07 03:33:03.071Z | 31.529° NE | 2026-05-07 03:36:03.071Z | 80.32° E | 36.788° | 2026-05-07 03:44:03.071Z | 148.666° SSE |
| 13 mins | 2026-05-07 05:26:03.071Z | 331.064° NNW | 2026-05-07 05:32:03.071Z | 278.493° WNW | 30.015° | 2026-05-07 05:39:03.071Z | 216.472° SW |
| 15 mins | 2026-05-07 16:29:03.071Z | 162.604° S | 2026-05-07 16:36:03.071Z | 82.897° E | 40.042° | 2026-05-07 16:44:03.071Z | 15.799° NNE |
| 13 mins | 2026-05-07 18:27:03.071Z | 238.097° WSW | 2026-05-07 18:33:03.071Z | 291.02° WNW | 26.956° | 2026-05-07 18:40:03.071Z | 347.995° N |
| 12 mins | 2026-05-08 02:40:03.071Z | 18.553° NNE | 2026-05-08 02:46:03.071Z | 68.988° E | 24.286° | 2026-05-08 02:52:03.071Z | 118.326° SE |
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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