GONETS M 15 (M25), 44906
Orbit data source: Space-Track
GONETS M 15 (M25), 44906 is a payload satellite owned by Gonets (CIS) in LEO that was launched on Thu, 26 Dec 2019 UTC via an ROKOT 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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44906 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 15 (M25)
1 44906U 19096B 25258.33650381 .00000029 00000-0 13685-3 0 9996
2 44906 82.5200 255.4164 0016888 58.3624 301.9101 12.42860568259506Epoch: 2025-09-15T08:04Z
TLE epoch observation values (Epoch: 2025-09-15T08:04:33.929Z)
Latitude
0.00002°
Longitude
139.73242°
Altitude
1,490.188 km
Speed
7.122 km/s
True Right ascension
17h 01m 39s
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
12:16:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,505.142 km
Perigee altitude
1,478.56 km
Semi-major axis
7,869.988 km
Eccentricity
0.00169
Inclination
82.52°
RAAN
255.4164°
Arg. of periapsis
58.3624°
True anomaly
301.74564°
Mean anomaly
301.9101°
Eccentric anomaly
301.82789°
Mean motion
3.10872 °/min
Orbital period
115.8 mins
BSTAR
0.00013685
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Other satellites on launch #96 in the year 2019 (2019-12-26 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 15 (M25) 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 | 2025-09-15 23:37:04.808Z | 151.253° SSE | 2025-09-15 23:45:04.808Z | 81.264° E | 32.743° | 2025-09-15 23:52:04.808Z | 23.187° NE |
| 14 mins | 2025-09-16 01:35:04.808Z | 222.313° SW | 2025-09-16 01:41:04.808Z | 280.037° WNW | 34.222° | 2025-09-16 01:49:04.808Z | 354.196° N |
| 9 mins | 2025-09-16 09:50:04.808Z | 30.798° NE | 2025-09-16 09:54:04.808Z | 61.907° ENE | 17.757° | 2025-09-16 09:59:04.808Z | 99.877° ESE |
| 15 mins | 2025-09-16 11:45:04.808Z | 352.157° N | 2025-09-16 11:52:04.808Z | 336.104° NNW | 44.963° | 2025-09-16 12:00:04.808Z | 175.339° S |
| 8 mins | 2025-09-16 13:44:04.808Z | 310.482° NW | 2025-09-16 13:48:04.808Z | 280.205° WNW | 16.05° | 2025-09-16 13:52:04.808Z | 251.129° W |
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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