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: 5 hours ago
TLE from 5 hours ago
0 GONETS M 18
1 46487U 20068B 26252.29325130 -.00000004 00000-0 -96604-4 0 9992
2 46487 82.4927 294.2732 0019439 204.9193 155.0950 12.42876239269596Epoch: 2026-09-09T07:02Z
TLE epoch observation values (Epoch: 2026-09-09T07:02:16.912Z)
Latitude
0.00001°
Longitude
-159.64466°
Altitude
1,511.021 km
Speed
7.103 km/s
True Right ascension
19h 37m 05s
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
04:15:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,507.084 km
Perigee altitude
1,476.487 km
Semi-major axis
7,869.923 km
Eccentricity
0.00194
Inclination
82.4927°
RAAN
294.2732°
Arg. of periapsis
204.9193°
True anomaly
155.1886°
Mean anomaly
155.095°
Eccentric anomaly
155.14182°
Mean motion
3.10876 °/min
Orbital period
115.8 mins
BSTAR
-0.000096604
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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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2026-09-09 13:27:21.561Z | 14.61° NNE | 2026-09-09 13:34:21.561Z | 75.074° E | 30.152° | 2026-09-09 13:40:21.561Z | 124.201° SE |
| 15 mins | 2026-09-09 15:24:21.561Z | 341.436° N | 2026-09-09 15:31:21.561Z | 263.251° W | 57.852° | 2026-09-09 15:39:21.561Z | 193.813° SSW |
| 13 mins | 2026-09-10 02:28:21.561Z | 139.8° SSE | 2026-09-10 02:34:21.561Z | 85.292° E | 35.509° | 2026-09-10 02:41:21.561Z | 26.47° NE |
| 15 mins | 2026-09-10 04:24:21.561Z | 216.148° SW | 2026-09-10 04:31:21.561Z | 293.844° NW | 49.127° | 2026-09-10 04:39:21.561Z | 358.105° 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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