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: 5 hours ago
TLE from 5 hours ago
0 METEOR M2-2
1 44387U 19038A 26278.95164488 .00000136 00000-0 78679-4 0 9998
2 44387 98.9277 267.9355 0002289 71.4685 288.6741 14.24390435377063Epoch: 2026-10-05T22:50Z
TLE epoch observation values (Epoch: 2026-10-05T22:50:22.117Z)
Latitude
-0.00011°
Longitude
-89.2798°
Altitude
812.93 km
Speed
7.447 km/s
True Right ascension
17h 51m 44s
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
22:11:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
809.351 km
Perigee altitude
806.061 km
Semi-major axis
7,185.843 km
Eccentricity
0.00023
Inclination
98.9277°
RAAN
267.9355°
Arg. of periapsis
71.4685°
True anomaly
288.64925°
Mean anomaly
288.6741°
Eccentric anomaly
288.66167°
Mean motion
3.56309 °/min
Orbital period
101.04 mins
BSTAR
0.000078679
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-10-06 11:14:44.608Z | 48.578° ENE | 2026-10-06 11:17:44.608Z | 86.839° E | 22.203° | 2026-10-06 11:21:44.608Z | 140.926° SSE |
| 8 mins | 2026-10-06 12:54:44.608Z | 352.972° N | 2026-10-06 12:57:44.608Z | 304.887° NW | 42.848° | 2026-10-06 13:02:44.608Z | 221.563° SW |
| 7 mins | 2026-10-06 22:35:44.608Z | 118.959° SE | 2026-10-06 22:38:44.608Z | 64.284° ENE | 35.122° | 2026-10-06 22:42:44.608Z | 7.208° NNE |
| 7 mins | 2026-10-07 00:15:44.608Z | 220.169° SW | 2026-10-07 00:18:44.608Z | 269.813° W | 28.017° | 2026-10-07 00:22:44.608Z | 321.286° NNW |
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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