GONETS M 19, 46488
Orbit data source: Space-Track
GONETS M 19, 46488 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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46488 intel report (Beta)
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Edit Public Description
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: 12 hours ago
TLE from 12 hours ago
0 GONETS M 19
1 46488U 20068C 25339.31181207 .00000021 00000-0 77772-4 0 9998
2 46488 82.4941 107.7245 0014433 110.8514 249.4113 12.42884662235165Epoch: 2025-12-05T07:29Z
TLE epoch observation values (Epoch: 2025-12-05T07:29:00.562Z)
Latitude
-0.00001°
Longitude
-78.88356°
Altitude
1,501.109 km
Speed
7.112 km/s
True Right ascension
07h 10m 53s
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
17:53:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,503.109 km
Perigee altitude
1,480.391 km
Semi-major axis
7,869.887 km
Eccentricity
0.00144
Inclination
82.4941°
RAAN
107.7245°
Arg. of periapsis
110.8514°
True anomaly
249.25657°
Mean anomaly
249.4113°
Eccentric anomaly
249.33393°
Mean motion
3.10878 °/min
Orbital period
115.8 mins
BSTAR
0.000077772
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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 19 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. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2025-12-05 21:39:02.370Z | 333.133° NNW | 2025-12-05 21:45:02.370Z | 278.578° WNW | 32.681° | 2025-12-05 21:53:02.370Z | 208.86° SW |
| 14 mins | 2025-12-06 08:42:02.370Z | 157.432° SSE | 2025-12-06 08:49:02.370Z | 82.89° E | 37.764° | 2025-12-06 08:56:02.370Z | 19.742° NNE |
| 13 mins | 2025-12-06 10:40:02.370Z | 234.599° WSW | 2025-12-06 10:46:02.370Z | 292.096° WNW | 29.42° | 2025-12-06 10:53:02.370Z | 349.974° N |
| 11 mins | 2025-12-06 18:54:02.370Z | 26.515° NE | 2025-12-06 18:59:02.370Z | 69.367° E | 21.975° | 2025-12-06 19:05:02.370Z | 115.337° 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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