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: 10 hours ago
TLE from 10 hours ago
0 GONETS M 19
1 46488U 20068C 26304.91222388 .00000086 00000-0 55154-3 0 9993
2 46488 82.4937 261.9753 0014628 105.8441 254.4252 12.42896819276236Epoch: 2026-10-31T21:53Z
TLE epoch observation values (Epoch: 2026-10-31T21:53:36.143Z)
Latitude
-0.00005°
Longitude
-106.63645°
Altitude
1,500.155 km
Speed
7.113 km/s
True Right ascension
17h 27m 54s
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
03:28:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,503.211 km
Perigee altitude
1,480.187 km
Semi-major axis
7,869.836 km
Eccentricity
0.00146
Inclination
82.4937°
RAAN
261.9753°
Arg. of periapsis
105.8441°
True anomaly
254.26381°
Mean anomaly
254.4252°
Eccentric anomaly
254.3445°
Mean motion
3.10881 °/min
Orbital period
115.8 mins
BSTAR
0.00055154
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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 08:10:07.805Z | 8.556° NNE | 2026-11-01 08:17:07.805Z | 70.95° E | 40.154° | 2026-11-01 08:25:07.805Z | 140.255° SSE |
| 14 mins | 2026-11-01 10:07:07.805Z | 336.585° NNW | 2026-11-01 10:14:07.805Z | 271.718° WNW | 43.357° | 2026-11-01 10:21:07.805Z | 207.942° SW |
| 14 mins | 2026-11-01 21:11:07.805Z | 152.694° SSE | 2026-11-01 21:17:07.805Z | 93.117° ESE | 47.165° | 2026-11-01 21:25:07.805Z | 19.849° NNE |
| 14 mins | 2026-11-01 23:08:07.805Z | 229.494° WSW | 2026-11-01 23:14:07.805Z | 285.279° WNW | 37.052° | 2026-11-01 23:22:07.805Z | 352.853° N |
| 11 mins | 2026-11-02 07:22:07.805Z | 24.236° NE | 2026-11-02 07:27:07.805Z | 64.115° ENE | 22.072° | 2026-11-02 07:33:07.805Z | 110.553° 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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