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: 14 hours ago
TLE from 14 hours ago
0 METEOR M2-2
1 44387U 19038A 26306.90905874 -.00000190 00000-0 -62029-4 0 9991
2 44387 98.9301 296.3428 0001420 23.6304 336.4939 14.24396553381042Epoch: 2026-11-02T21:49Z
TLE epoch observation values (Epoch: 2026-11-02T21:49:02.675Z)
Latitude
-0.00002°
Longitude
-73.09766°
Altitude
812.499 km
Speed
7.448 km/s
True Right ascension
19h 45m 22s
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
07:20:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
808.706 km
Perigee altitude
806.665 km
Semi-major axis
7,185.823 km
Eccentricity
0.00014
Inclination
98.9301°
RAAN
296.3428°
Arg. of periapsis
23.6304°
True anomaly
336.48741°
Mean anomaly
336.4939°
Eccentric anomaly
336.49065°
Mean motion
3.5631 °/min
Orbital period
101.04 mins
BSTAR
-0.000062029
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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 | 2026-11-03 11:53:30.987Z | 28.888° NE | 2026-11-03 11:57:30.987Z | 90.225° ESE | 47.704° | 2026-11-03 12:02:30.987Z | 173.008° S |
| 6 mins | 2026-11-03 13:34:30.987Z | 334.355° NNW | 2026-11-03 13:37:30.987Z | 292.37° WNW | 21.723° | 2026-11-03 13:40:30.987Z | 253.528° W |
| 9 mins | 2026-11-03 23:13:30.987Z | 156.852° SSE | 2026-11-03 23:17:30.987Z | 102.538° ESE | 72.667° | 2026-11-03 23:22:30.987Z | 350.448° 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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