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: 11 hours ago
TLE from 11 hours ago
0 METEOR M2-2
1 44387U 19038A 25312.17363385 .00000244 00000-0 12537-3 0 9997
2 44387 98.8936 291.4854 0000612 353.0260 7.0909 14.24268247329832Epoch: 2025-11-08T04:10Z
TLE epoch observation values (Epoch: 2025-11-08T04:10:01.964Z)
Latitude
-0.0001°
Longitude
-178.62981°
Altitude
813.432 km
Speed
7.447 km/s
True Right ascension
19h 25m 56s
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
11:23:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
808.556 km
Perigee altitude
807.676 km
Semi-major axis
7,186.253 km
Eccentricity
0.00006
Inclination
98.8936°
RAAN
291.4854°
Arg. of periapsis
353.026°
True anomaly
7.09177°
Mean anomaly
7.0909°
Eccentric anomaly
7.09133°
Mean motion
3.56278 °/min
Orbital period
101.04 mins
BSTAR
0.00012537
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-08 21:12:33.054Z | 87.149° E | 2025-11-08 21:14:33.054Z | 63.867° ENE | 13.73° | 2025-11-08 21:16:33.054Z | 39.38° NE |
| 8 mins | 2025-11-08 22:50:33.054Z | 172.861° S | 2025-11-08 22:54:33.054Z | 306.774° NW | 43.203° | 2025-11-08 22:58:33.054Z | 342.265° N |
| 8 mins | 2025-11-09 11:06:33.054Z | 33.393° NE | 2025-11-09 11:10:33.054Z | 100.591° ESE | 33.779° | 2025-11-09 11:14:33.054Z | 165.174° S |
| 6 mins | 2025-11-09 12:47:33.054Z | 333.398° NNW | 2025-11-09 12:50:33.054Z | 287.138° WNW | 22.179° | 2025-11-09 12:53:33.054Z | 248.088° 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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