GONETS M 14 (M24), 44905
Orbit data source: Space-Track
GONETS M 14 (M24), 44905 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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44905 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: 14 hours ago
TLE from 14 hours ago
0 GONETS M 14 (M24)
1 44905U 19096A 25258.23018589 .00000035 00000-0 17833-3 0 9998
2 44905 82.5181 255.0704 0014515 37.8326 322.3771 12.42896687259528Epoch: 2025-09-15T05:31Z
TLE epoch observation values (Epoch: 2025-09-15T05:31:28.06Z)
Latitude
-0.00005°
Longitude
177.76565°
Altitude
1,488.002 km
Speed
7.124 km/s
True Right ascension
17h 00m 16s
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
12:17:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,503.121 km
Perigee altitude
1,480.275 km
Semi-major axis
7,869.835 km
Eccentricity
0.00145
Inclination
82.5181°
RAAN
255.0704°
Arg. of periapsis
37.8326°
True anomaly
322.27542°
Mean anomaly
322.3771°
Eccentric anomaly
322.32627°
Mean motion
3.10881 °/min
Orbital period
115.8 mins
BSTAR
0.00017833
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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 14 (M24) 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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-09-15 23:01:45.769Z | 127.181° SE | 2025-09-15 23:07:45.769Z | 80.802° E | 21.901° | 2025-09-15 23:13:45.769Z | 34.492° NE |
| 15 mins | 2025-09-16 00:56:45.769Z | 198.523° SSW | 2025-09-16 01:03:45.769Z | 282.121° WNW | 43.2° | 2025-09-16 01:11:45.769Z | 2.758° NNE |
| 6 mins | 2025-09-16 02:59:45.769Z | 283.331° WNW | 2025-09-16 03:02:45.769Z | 304.967° NW | 12.65° | 2025-09-16 03:05:45.769Z | 325.916° NNW |
| 15 mins | 2025-09-16 11:07:45.769Z | 3.176° NNE | 2025-09-16 11:14:45.769Z | 79.743° E | 40.288° | 2025-09-16 11:22:45.769Z | 155.1° SSE |
| 12 mins | 2025-09-16 13:05:45.769Z | 323.078° NNW | 2025-09-16 13:10:45.769Z | 278.828° WNW | 26.31° | 2025-09-16 13:17:45.769Z | 222.543° SW |
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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