METEOR M2, 40069
Orbit data source: Space-Track
METEOR M2, 40069 is a Commonwealth of Independent States-origin payload satellite in SSO that was launched on Tue, 08 Jul 2014 UTC via a SOYUZ-2-1B launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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40069 intel report (Beta)
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METEOR M2 radio frequencies
METEOR M2 details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 9 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 9 hours ago
0 METEOR M2
1 40069U 14037A 24361.10789074 .00000392 00000-0 19953-3 0 9990
2 40069 98.4524 346.9419 0006186 150.5497 209.6031 14.21172190542887Epoch: 2024-12-26T02:35Z
Definitive object data (Epoch: 2024-12-26T02:35:21.759Z)
| Latitude | 0° |
| Longitude | -146.99079° |
| Altitude | 828.189 km |
| Speed | 7.437 km/s |
| True Right ascension | 23h 07m 46s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 50.17006° |
| Longitude | -156.85259° |
| Altitude | 830.032 km |
| Speed | 7.442 km/s |
| Apparent Right ascension | 22h 33m 14s |
| Apparent Declination | 8° 36' 32" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 10:37:53 |
| Azimuth | 1.533° NNE |
| Elevation | -41.463° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 822.988 km |
| Perigee altitude | 814.084 km |
| Semi-major axis | 7,196.673 km |
| Eccentricity | 0.0006186 |
| Inclination | 98.4524° |
| RAAN | 346.9419° |
| Arg. of periapsis | 150.5497° |
| True anomaly | 209.56811° |
| Mean anomaly | 209.6031° |
| Eccentric anomaly | 209.5856° |
| Mean motion | 3.55505 °/min |
| BSTAR | 0.00019953 |
| Orbital period | 101.26 mins |
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Other satellites on launch #37 in the year 2014 (2014-07-08 UTC)
| METEOR M2, 40069 |
| MKA PN2 (RELEK), 40070 |
| DX 1, 40071 |
| SKYSAT 2, 40072 |
| DUMMY SAT, 40073 |
| UKUBE 1, 40074 |
| AISSAT 2, 40075 |
| TDS 1, 40076 |
| SL-4 R/B, 40077 (Decayed) |
| FREGAT DEB, 40078 |
METEOR M2 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 11:37:33.929Z | 30.193° NE | 2024-12-26 11:41:33.929Z | 88.083° E | 34.152° | 2024-12-26 11:46:33.929Z | 168.51° S |
| 6 mins | 2024-12-26 13:19:33.929Z | 328.167° NNW | 2024-12-26 13:21:33.929Z | 297.947° NW | 21.899° | 2024-12-26 13:25:33.929Z | 245.615° WSW |
| 9 mins | 2024-12-26 22:59:33.929Z | 151.45° SSE | 2024-12-26 23:03:33.929Z | 71.764° E | 42.3° | 2024-12-26 23:08:33.929Z | 353.318° N |
| 4 mins | 2024-12-27 00:42:33.929Z | 250.134° W | 2024-12-27 00:44:33.929Z | 275.197° WNW | 14.346° | 2024-12-27 00:46:33.929Z | 298.492° NW |
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