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). Payloads include a variety of satellites, spacecraft, and rockets 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
METEOR M2-2 details
Identifier | |
Orbit | SSO |
Last TLE update | 8 hours ago |
Origin | |
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 | Payload Rocket body Debris |
Shape & HBR | Cyl + 2 Pan, 14 m |
Radar Cross Section | 26.744 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 8 hours ago
0 METEOR M2-2
1 44387U 19038A 24361.11450103 .00000367 00000-0 17906-3 0 9990
2 44387 98.8537 331.3706 0002133 109.5704 250.5705 14.24098450284708
Epoch: 2024-12-26T02:44Z
Definitive object data (Epoch: 2024-12-26T02:44:52.889Z)
Latitude | 0.00003° |
Longitude | -164.94832° |
Altitude | 814.951 km |
Speed | 7.445 km/s |
True Right ascension | 22h 05m 28s |
True Declination | 0° 00' 00" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | -14.91937° |
Longitude | -162.23151° |
Altitude | 818.408 km |
Speed | 7.443 km/s |
Apparent Right ascension | 22h 21m 05s |
Apparent Declination | -26° 31' 05" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 10:27:49 |
Azimuth | 6.477° NNE |
Elevation | -76.529° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 810.218 km |
Perigee altitude | 807.153 km |
Semi-major axis | 7,186.822 km |
Eccentricity | 0.0002133 |
Inclination | 98.8537° |
RAAN | 331.3706° |
Arg. of periapsis | 109.5704° |
True anomaly | 250.54745° |
Mean anomaly | 250.5705° |
Eccentric anomaly | 250.55898° |
Mean motion | 3.56236 °/min |
BSTAR | 0.00017906 |
Orbital period | 101.06 mins |
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Other satellites on launch #38 in the year 2019 (2019-07-05 UTC)
METEOR M2-2 Visibility forecast
Observer location: undefined°, undefined
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 | 2024-12-26 11:44:31.661Z | 359.966° N | 2024-12-26 11:49:31.661Z | 284.859° WNW | 34.819° | 2024-12-26 11:53:31.661Z | 222.852° SW |
8 mins | 2024-12-26 21:26:31.661Z | 123.327° SE | 2024-12-26 21:29:31.661Z | 77.3° E | 29.356° | 2024-12-26 21:34:31.661Z | 4.971° NNE |
7 mins | 2024-12-26 23:06:31.661Z | 214.283° SW | 2024-12-26 23:09:31.661Z | 258.69° W | 25.401° | 2024-12-26 23:13:31.661Z | 317.606° NNW |
Authenticating...
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