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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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: 3 hours ago
TLE from 3 hours ago
0 GONETS M 19
1 46488U 20068C 26305.23420995 .00000023 00000-0 92530-4 0 9994
2 46488 82.4938 261.7750 0014636 105.1915 255.0784 12.42896572276277Epoch: 2026-11-01T05:37Z
TLE epoch observation values (Epoch: 2026-11-01T05:37:15.739Z)
Latitude
-0.00006°
Longitude
136.9309°
Altitude
1,500.031 km
Speed
7.113 km/s
True Right ascension
17h 27m 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
04:41:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,503.218 km
Perigee altitude
1,480.181 km
Semi-major axis
7,869.837 km
Eccentricity
0.00146
Inclination
82.4938°
RAAN
261.775°
Arg. of periapsis
105.1915°
True anomaly
254.91642°
Mean anomaly
255.0784°
Eccentric anomaly
254.9974°
Mean motion
3.10881 °/min
Orbital period
115.8 mins
BSTAR
0.00009253
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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. |
|---|---|---|---|---|---|---|---|
| 15 mins | 2026-11-01 10:06:40.117Z | 338.005° N | 2026-11-01 10:13:40.117Z | 279.485° WNW | 43.118° | 2026-11-01 10:21:40.117Z | 206.285° SW |
| 14 mins | 2026-11-01 21:10:40.117Z | 154.289° SSE | 2026-11-01 21:17:40.117Z | 82.968° E | 47.133° | 2026-11-01 21:24:40.117Z | 21.052° NNE |
| 14 mins | 2026-11-01 23:07:40.117Z | 227.43° WSW | 2026-11-01 23:14:40.117Z | 292.834° NW | 36.951° | 2026-11-01 23:21:40.117Z | 351.167° N |
| 10 mins | 2026-11-02 07:22:40.117Z | 27.576° NE | 2026-11-02 07:27:40.117Z | 69.145° E | 22.005° | 2026-11-02 07:32:40.117Z | 107.99° ESE |
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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