METEOR M2-2, 44387
Orbit data source: Space-Track
METEOR M2-2, 44387 is a Commonwealth of Independent States-origin payload satellite in SSO that was launched on Fri, 05 Jul 2019 UTC via a SOYUZ-2-1B launch vehicle from the Vostochny Cosmodrome (VOSTO). 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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44387 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
VNIIEM
Mission
Partially operational Civil Weather
Bus & Motor
RESURS-O, Unknown motor
Mass
2,879 kg wet, ~2,600 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + 2 Pan, 7.0 m
Radar Cross Section
26.744 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 METEOR M2-2
1 44387U 19038A 25287.93691554 .00000231 00000-0 11978-3 0 9998
2 44387 98.8903 266.9638 0001799 42.1857 317.9460 14.24253767326381Epoch: 2025-10-14T22:29Z
TLE epoch observation values (Epoch: 2025-10-14T22:29:09.502Z)
Latitude
0.00002°
Longitude
-94.04398°
Altitude
812.957 km
Speed
7.447 km/s
True Right ascension
17h 47m 51s
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
08:41:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
809.457 km
Perigee altitude
806.872 km
Semi-major axis
7,186.301 km
Eccentricity
0.00018
Inclination
98.8903°
RAAN
266.9638°
Arg. of periapsis
42.1857°
True anomaly
317.93219°
Mean anomaly
317.946°
Eccentric anomaly
317.93909°
Mean motion
3.56275 °/min
Orbital period
101.05 mins
BSTAR
0.00011978
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Other satellites on launch #38 in the year 2019 (2019-07-05 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.METEOR M2-2 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-10-15 22:12:56.698Z | 143.189° SSE | 2025-10-15 22:16:56.698Z | 81.167° E | 38.003° | 2025-10-15 22:21:56.698Z | 357.493° N |
| 5 mins | 2025-10-15 23:54:56.698Z | 235.033° WSW | 2025-10-15 23:56:56.698Z | 261.341° W | 17.743° | 2025-10-15 23:59:56.698Z | 301.454° NW |
| 6 mins | 2025-10-16 10:30:56.698Z | 60.374° ENE | 2025-10-16 10:32:56.698Z | 87.604° E | 18.997° | 2025-10-16 10:36:56.698Z | 138.789° SSE |
| 8 mins | 2025-10-16 12:09:56.698Z | 355.344° N | 2025-10-16 12:12:56.698Z | 306.597° NW | 36.092° | 2025-10-16 12:17:56.698Z | 218.292° 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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