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: 10 hours ago
TLE from 10 hours ago
0 METEOR M2-2
1 44387U 19038A 25335.84807917 .00000190 00000-0 10235-3 0 9993
2 44387 98.8961 315.4442 0000798 171.6466 188.4726 14.24283765333206Epoch: 2025-12-01T20:21Z
TLE epoch observation values (Epoch: 2025-12-01T20:21:14.040Z)
Latitude
0.00002°
Longitude
-60.806°
Altitude
814.384 km
Speed
7.446 km/s
True Right ascension
21h 01m 46s
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
03:48:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
808.637 km
Perigee altitude
807.49 km
Semi-major axis
7,186.201 km
Eccentricity
0.00008
Inclination
98.8961°
RAAN
315.4442°
Arg. of periapsis
171.6466°
True anomaly
188.47125°
Mean anomaly
188.4726°
Eccentric anomaly
188.47193°
Mean motion
3.56282 °/min
Orbital period
101.04 mins
BSTAR
0.00010235
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-02 10:27:44.352Z | 59.897° ENE | 2025-12-02 10:30:44.352Z | 98.312° ESE | 16.214° | 2025-12-02 10:32:44.352Z | 123.296° SE |
| 8 mins | 2025-12-02 12:06:44.352Z | 1.042° NNE | 2025-12-02 12:10:44.352Z | 276.78° WNW | 39.833° | 2025-12-02 12:14:44.352Z | 213.394° SW |
| 7 mins | 2025-12-02 21:47:44.352Z | 114.319° SE | 2025-12-02 21:50:44.352Z | 71.32° E | 24.724° | 2025-12-02 21:54:44.352Z | 14° NNE |
| 7 mins | 2025-12-02 23:27:44.352Z | 208.151° SW | 2025-12-02 23:30:44.352Z | 262.966° W | 30.774° | 2025-12-02 23:34:44.352Z | 324.292° NNW |
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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