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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METEOR M2-2 radio frequencies
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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: 7 hours ago
TLE from 7 hours ago
0 METEOR M2-2
1 44387U 19038A 25261.94362384 .00000134 00000-0 77857-4 0 9998
2 44387 98.8857 240.6745 0002368 82.4119 277.7328 14.24236606322686Epoch: 2025-09-18T22:38Z
TLE epoch observation values (Epoch: 2025-09-18T22:38:49.099Z)
Latitude
-0.00006°
Longitude
-97.12804°
Altitude
813.746 km
Speed
7.446 km/s
True Right ascension
16h 02m 41s
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
22:27:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
809.924 km
Perigee altitude
806.52 km
Semi-major axis
7,186.359 km
Eccentricity
0.00024
Inclination
98.8857°
RAAN
240.6745°
Arg. of periapsis
82.4119°
True anomaly
277.70591°
Mean anomaly
277.7328°
Eccentric anomaly
277.71936°
Mean motion
3.5627 °/min
Orbital period
101.05 mins
BSTAR
0.000077857
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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 | 2025-09-19 11:01:48.820Z | 28.988° NE | 2025-09-19 11:06:48.820Z | 109.053° ESE | 34.148° | 2025-09-19 11:10:48.820Z | 167.56° S |
| 6 mins | 2025-09-19 12:43:48.820Z | 329.944° NNW | 2025-09-19 12:45:48.820Z | 300.022° NW | 21.833° | 2025-09-19 12:49:48.820Z | 246.616° WSW |
| 9 mins | 2025-09-19 22:22:48.820Z | 151.935° SSE | 2025-09-19 22:26:48.820Z | 61.614° ENE | 42.625° | 2025-09-19 22:31:48.820Z | 351.936° N |
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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