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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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: 12 hours ago
TLE from 12 hours ago
0 METEOR M2-2
1 44387U 19038A 26235.61036624 -.00000139 00000-0 -40133-4 0 9993
2 44387 98.9212 223.9105 0001492 134.8401 225.2898 14.24380095370897Epoch: 2026-08-23T14:38Z
TLE epoch observation values (Epoch: 2026-08-23T14:38:55.643Z)
Latitude
-0.00007°
Longitude
32.27472°
Altitude
814.246 km
Speed
7.446 km/s
True Right ascension
14h 55m 38s
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
18:11:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
808.813 km
Perigee altitude
806.669 km
Semi-major axis
7,185.878 km
Eccentricity
0.00015
Inclination
98.9212°
RAAN
223.9105°
Arg. of periapsis
134.8401°
True anomaly
225.27765°
Mean anomaly
225.2898°
Eccentric anomaly
225.28373°
Mean motion
3.56306 °/min
Orbital period
101.04 mins
BSTAR
-0.000040133
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-08-24 11:28:39.329Z | 39.426° NE | 2026-08-24 11:32:39.329Z | 103.226° ESE | 28.737° | 2026-08-24 11:36:39.329Z | 158.658° S |
| 7 mins | 2026-08-24 13:08:39.329Z | 345.489° N | 2026-08-24 13:11:39.329Z | 303.583° NW | 26.079° | 2026-08-24 13:15:39.329Z | 241.018° WSW |
| 9 mins | 2026-08-24 22:48:39.329Z | 142.232° SSE | 2026-08-24 22:52:39.329Z | 68.62° E | 38.357° | 2026-08-24 22:57:39.329Z | 356.43° N |
| 5 mins | 2026-08-25 00:30:39.329Z | 238.7° WSW | 2026-08-25 00:32:39.329Z | 265.913° W | 17.734° | 2026-08-25 00:35:39.329Z | 304.439° NW |
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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