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: 7 hours ago
TLE from 7 hours ago
0 METEOR M2-2
1 44387U 19038A 26171.26525613 .00000060 00000-0 45595-4 0 9992
2 44387 98.9149 158.5968 0001978 43.4360 316.6974 14.24366747361735Epoch: 2026-06-20T06:21Z
TLE epoch observation values (Epoch: 2026-06-20T06:21:58.129Z)
Latitude
-0.00001°
Longitude
154.62224°
Altitude
812.501 km
Speed
7.448 km/s
True Right ascension
10h 34m 23s
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
00:33:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
809.207 km
Perigee altitude
806.364 km
Semi-major axis
7,185.922 km
Eccentricity
0.0002
Inclination
98.9149°
RAAN
158.5968°
Arg. of periapsis
43.436°
True anomaly
316.68185°
Mean anomaly
316.6974°
Eccentric anomaly
316.68963°
Mean motion
3.56303 °/min
Orbital period
101.04 mins
BSTAR
0.000045595
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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 | 2026-06-20 13:41:51.231Z | 323.698° NNW | 2026-06-20 13:43:51.231Z | 300.029° NW | 13.363° | 2026-06-20 13:45:51.231Z | 276.438° WNW |
| 4 mins | 2026-06-20 21:43:51.231Z | 81.165° E | 2026-06-20 21:45:51.231Z | 55.059° ENE | 15.218° | 2026-06-20 21:47:51.231Z | 31.037° NE |
| 9 mins | 2026-06-20 23:20:51.231Z | 177.454° S | 2026-06-20 23:24:51.231Z | 270.907° WNW | 42.702° | 2026-06-20 23:29:51.231Z | 340.779° N |
| 8 mins | 2026-06-21 11:37:51.231Z | 35.16° NE | 2026-06-21 11:40:51.231Z | 91.319° ESE | 36.202° | 2026-06-21 11:45:51.231Z | 172.691° S |
| 6 mins | 2026-06-21 13:17:51.231Z | 334.353° NNW | 2026-06-21 13:20:51.231Z | 291.976° WNW | 20.399° | 2026-06-21 13:23:51.231Z | 253.021° 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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