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: 15 hours ago
TLE from 15 hours ago
0 GONETS M 14 (M24)
1 44905U 19096A 25311.27727009 .00000047 00000-0 26710-3 0 9993
2 44905 82.5255 222.1796 0012767 281.1767 78.7878 12.42898689266113Epoch: 2025-11-07T06:39Z
TLE epoch observation values (Epoch: 2025-11-07T06:39:16.135Z)
Latitude
0.00003°
Longitude
75.63883°
Altitude
1,495.097 km
Speed
7.117 km/s
True Right ascension
14h 48m 43s
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
17:41:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,501.737 km
Perigee altitude
1,481.642 km
Semi-major axis
7,869.826 km
Eccentricity
0.00128
Inclination
82.5255°
RAAN
222.1796°
Arg. of periapsis
281.1767°
True anomaly
78.93135°
Mean anomaly
78.7878°
Eccentric anomaly
78.85957°
Mean motion
3.10882 °/min
Orbital period
115.8 mins
BSTAR
0.0002671
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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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2025-11-08 04:31:00.038Z | 14.029° NNE | 2025-11-08 04:38:00.038Z | 68.766° E | 24.113° | 2025-11-08 04:44:00.038Z | 117.462° SE |
| 15 mins | 2025-11-08 06:28:00.038Z | 345.339° N | 2025-11-08 06:35:00.038Z | 281.463° WNW | 42.366° | 2025-11-08 06:43:00.038Z | 189.377° SSW |
| 12 mins | 2025-11-08 17:33:00.038Z | 133.318° SE | 2025-11-08 17:39:00.038Z | 79.962° E | 26.987° | 2025-11-08 17:45:00.038Z | 30.874° NE |
| 15 mins | 2025-11-08 19:28:00.038Z | 208.685° SW | 2025-11-08 19:35:00.038Z | 282.853° WNW | 39.762° | 2025-11-08 19:43:00.038Z | 358.897° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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