METEOR M2, 40069
Orbit data source: Space-Track
METEOR M2, 40069 is a Commonwealth of Independent States-origin payload satellite in LEO 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 | LEO |
| Last TLE update | 6 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 6 hours ago
0 METEOR M2
1 40069U 14037A 24339.14155395 .00000433 00000-0 21845-3 0 9991
2 40069 98.4508 325.9213 0004943 215.6614 144.4234 14.21154828539763Epoch: 2024-12-04T03:23Z
Definitive object data (Epoch: 2024-12-04T03:23:50.261Z)
| Latitude | -0.00004° |
| Longitude | -158.47908° |
| Altitude | 827.27 km |
| Speed | 7.438 km/s |
| True Right ascension | 21h 43m 41s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 17.88871° |
| Longitude | 24.48743° |
| Altitude | 821.666 km |
| Speed | 7.445 km/s |
| Apparent Right ascension | 12h 57m 49s |
| Apparent Declination | -22° 12' 37" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 07:07:49 |
| Azimuth | 108.854° ESE |
| Elevation | -12.215° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 822.152 km |
| Perigee altitude | 815.037 km |
| Semi-major axis | 7,196.732 km |
| Eccentricity | 0.0004943 |
| Inclination | 98.4508° |
| RAAN | 325.9213° |
| Arg. of periapsis | 215.6614° |
| True anomaly | 144.45634° |
| Mean anomaly | 144.4234° |
| Eccentric anomaly | 144.43987° |
| Mean motion | 3.555 °/min |
| BSTAR | 0.00021845 |
| Orbital period | 101.27 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2024-12-04 10:47:34.320Z | 70.054° E | 2024-12-04 10:49:34.320Z | 93.735° ESE | 12.927° | 2024-12-04 10:51:34.320Z | 116.396° SE |
| 8 mins | 2024-12-04 12:26:34.320Z | 5.517° NNE | 2024-12-04 12:29:34.320Z | 315.072° NNW | 43.192° | 2024-12-04 12:34:34.320Z | 203.298° SW |
| 6 mins | 2024-12-04 22:09:34.320Z | 95.454° ESE | 2024-12-04 22:11:34.320Z | 66.58° ENE | 20.449° | 2024-12-04 22:15:34.320Z | 16.809° NNE |
| 9 mins | 2024-12-04 23:47:34.320Z | 191.565° SSW | 2024-12-04 23:51:34.320Z | 263.897° W | 36.684° | 2024-12-04 23:56:34.320Z | 334.87° NNW |
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