GONETS M 16 (M26), 44907
Orbit data source: Space-Track
GONETS M 16 (M26), 44907 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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44907 intel report (Beta)
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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 16 (M26)
1 44907U 19096C 26172.53113285 .00000008 00000-0 -15213-4 0 9990
2 44907 82.5198 81.3603 0009958 204.1673 155.8941 12.42891888294171Epoch: 2026-06-21T12:44Z
TLE epoch observation values (Epoch: 2026-06-21T12:44:49.878Z)
Latitude
0.00002°
Longitude
-19.57759°
Altitude
1,504.226 km
Speed
7.109 km/s
True Right ascension
05h 25m 26s
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
23:19:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,499.555 km
Perigee altitude
1,483.882 km
Semi-major axis
7,869.855 km
Eccentricity
0.001
Inclination
82.5198°
RAAN
81.3603°
Arg. of periapsis
204.1673°
True anomaly
155.94065°
Mean anomaly
155.8941°
Eccentric anomaly
155.91738°
Mean motion
3.1088 °/min
Orbital period
115.8 mins
BSTAR
-0.000015213
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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 16 (M26) 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 | 2026-06-22 17:49:10.210Z | 156.478° SSE | 2026-06-22 17:56:10.210Z | 93.275° ESE | 36.653° | 2026-06-22 18:04:10.210Z | 19.613° NNE |
| 14 mins | 2026-06-22 19:47:10.210Z | 230.059° WSW | 2026-06-22 19:53:10.210Z | 285.239° WNW | 30.82° | 2026-06-22 20:01:10.210Z | 352.532° N |
| 11 mins | 2026-06-23 04:01:10.210Z | 23.713° NE | 2026-06-23 04:06:10.210Z | 63.546° ENE | 20.914° | 2026-06-23 04:12:10.210Z | 110.629° ESE |
| 15 mins | 2026-06-23 05:57:10.210Z | 348.204° N | 2026-06-23 06:04:10.210Z | 261.906° W | 44.228° | 2026-06-23 06:12:10.210Z | 182.418° SSW |
| 5 mins | 2026-06-23 07:57:10.210Z | 300.761° NW | 2026-06-23 07:59:10.210Z | 286.349° WNW | 12.906° | 2026-06-23 08:02:10.210Z | 264.95° 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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