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: 19 hours ago
TLE from 19 hours ago
0 GONETS M 19
1 46488U 20068C 25261.30897297 .00000012 00000-0 16542-4 0 9992
2 46488 82.4987 156.2601 0012906 283.6717 76.2926 12.42861793225478Epoch: 2025-09-18T07:24Z
TLE epoch observation values (Epoch: 2025-09-18T07:24:55.264Z)
Latitude
0.00003°
Longitude
47.55741°
Altitude
1,494.799 km
Speed
7.118 km/s
True Right ascension
10h 25m 02s
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
18:53:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,502.003 km
Perigee altitude
1,481.689 km
Semi-major axis
7,869.983 km
Eccentricity
0.00129
Inclination
82.4987°
RAAN
156.2601°
Arg. of periapsis
283.6717°
True anomaly
76.43633°
Mean anomaly
76.2926°
Eccentric anomaly
76.36446°
Mean motion
3.10873 °/min
Orbital period
115.8 mins
BSTAR
0.000016542
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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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2025-09-19 03:21:12.068Z | 16.934° NNE | 2025-09-19 03:27:12.068Z | 63.268° ENE | 22.981° | 2025-09-19 03:34:12.068Z | 118.2° SE |
| 15 mins | 2025-09-19 05:18:12.068Z | 345.865° N | 2025-09-19 05:25:12.068Z | 264.163° W | 43.218° | 2025-09-19 05:33:12.068Z | 186.53° SSW |
| 12 mins | 2025-09-19 16:23:12.068Z | 129.289° SE | 2025-09-19 16:28:12.068Z | 86.434° E | 25.715° | 2025-09-19 16:35:12.068Z | 29.904° NE |
| 16 mins | 2025-09-19 18:17:12.068Z | 204.959° SW | 2025-09-19 18:25:12.068Z | 294.914° NW | 40.551° | 2025-09-19 18:33:12.068Z | 0.723° 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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