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: 1 day ago
TLE from 1 day ago
0 GONETS M 19
1 46488U 20068C 25322.48787410 .00000038 00000-0 20512-3 0 9993
2 46488 82.4921 118.1941 0014206 145.3383 214.8625 12.42883978233078Epoch: 2025-11-18T11:42Z
TLE epoch observation values (Epoch: 2025-11-18T11:42:32.322Z)
Latitude
-0.00003°
Longitude
-115.21383°
Altitude
1,506.284 km
Speed
7.107 km/s
True Right ascension
07h 52m 46s
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
16:10:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,502.933 km
Perigee altitude
1,480.573 km
Semi-major axis
7,869.89 km
Eccentricity
0.00142
Inclination
82.4921°
RAAN
118.1941°
Arg. of periapsis
145.3383°
True anomaly
214.76958°
Mean anomaly
214.8625°
Eccentric anomaly
214.81603°
Mean motion
3.10878 °/min
Orbital period
115.8 mins
BSTAR
0.00020512
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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 | 2025-11-19 21:09:55.744Z | 9.927° NNE | 2025-11-19 21:16:55.744Z | 69.654° E | 30.273° | 2025-11-19 21:23:55.744Z | 132.219° SE |
| 15 mins | 2025-11-19 23:06:55.744Z | 339.113° N | 2025-11-19 23:13:55.744Z | 273.898° WNW | 36.917° | 2025-11-19 23:21:55.744Z | 201.074° SSW |
| 14 mins | 2025-11-20 10:10:55.744Z | 148.551° SSE | 2025-11-20 10:16:55.744Z | 94.502° ESE | 33.633° | 2025-11-20 10:24:55.744Z | 22.185° NNE |
| 14 mins | 2025-11-20 12:07:55.744Z | 224.548° SW | 2025-11-20 12:13:55.744Z | 282.862° WNW | 33.612° | 2025-11-20 12:21:55.744Z | 354.095° 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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