GONETS M 20, 47227
Orbit data source: Space-Track
GONETS M 20, 47227 is a payload satellite owned by Gonets (CIS) in LEO that was launched on Thu, 03 Dec 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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47227 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 20
1 47227U 20091A 26172.51386189 -.00000020 00000-0 -21351-3 0 9992
2 47227 82.5052 299.7464 0021420 168.5716 191.5854 12.42893542251618Epoch: 2026-06-21T12:19Z
TLE epoch observation values (Epoch: 2026-06-21T12:19:57.667Z)
Latitude
-0.00004°
Longitude
-154.95693°
Altitude
1,513.584 km
Speed
7.101 km/s
True Right ascension
19h 58m 59s
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
21:29:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,508.569 km
Perigee altitude
1,474.855 km
Semi-major axis
7,869.849 km
Eccentricity
0.00214
Inclination
82.5052°
RAAN
299.7464°
Arg. of periapsis
168.5716°
True anomaly
191.53623°
Mean anomaly
191.5854°
Eccentric anomaly
191.5608°
Mean motion
3.10881 °/min
Orbital period
115.8 mins
BSTAR
-0.00021351
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Other satellites on launch #91 in the year 2020 (2020-12-03 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 20 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-22 11:44:50.039Z | 287.595° WNW | 2026-06-22 11:46:50.039Z | 301.343° NW | 11.358° | 2026-06-22 11:48:50.039Z | 315.251° NNW |
| 16 mins | 2026-06-22 19:51:50.039Z | 359.853° N | 2026-06-22 19:58:50.039Z | 63.438° ENE | 41.693° | 2026-06-22 20:07:50.039Z | 160.007° S |
| 12 mins | 2026-06-22 21:49:50.039Z | 324.118° NNW | 2026-06-22 21:55:50.039Z | 273.42° WNW | 23.759° | 2026-06-22 22:01:50.039Z | 227.573° WSW |
| 5 mins | 2026-06-23 07:01:50.039Z | 88.264° E | 2026-06-23 07:03:50.039Z | 73.933° E | 12.678° | 2026-06-23 07:06:50.039Z | 53.041° ENE |
| 15 mins | 2026-06-23 08:51:50.039Z | 175.834° S | 2026-06-23 08:58:50.039Z | 99.776° ESE | 44.045° | 2026-06-23 09:06:50.039Z | 11.57° NNE |
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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