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). 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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40069 intel report (Beta)
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Edit Public Description
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: 19 hours ago
TLE from 19 hours ago
0 METEOR M2
1 40069U 14037A 25301.62548176 .00000256 00000-0 13665-3 0 9991
2 40069 98.4856 280.9501 0005745 1.6443 358.4753 14.21359333586429Epoch: 2025-10-28T15:00Z
TLE epoch observation values (Epoch: 2025-10-28T15:00:41.624Z)
Latitude
0.00002°
Longitude
18.56638°
Altitude
819.548 km
Speed
7.446 km/s
True Right ascension
18h 43m 48s
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
05:30:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
822.04 km
Perigee altitude
813.771 km
Semi-major axis
7,196.042 km
Eccentricity
0.00057
Inclination
98.4856°
RAAN
280.9501°
Arg. of periapsis
1.6443°
True anomaly
358.47355°
Mean anomaly
358.4753°
Eccentric anomaly
358.47442°
Mean motion
3.55552 °/min
Orbital period
101.25 mins
BSTAR
0.00013665
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Other satellites on launch #37 in the year 2014 (2014-07-08 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 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-29 10:13:12.037Z | 62.546° ENE | 2025-10-29 10:15:12.037Z | 85.235° E | 13.333° | 2025-10-29 10:18:12.037Z | 119.783° SE |
| 9 mins | 2025-10-29 11:52:12.037Z | 6.442° NNE | 2025-10-29 11:56:12.037Z | 285.948° WNW | 43.321° | 2025-10-29 12:01:12.037Z | 203.792° SW |
| 6 mins | 2025-10-29 21:35:12.037Z | 102.779° ESE | 2025-10-29 21:38:12.037Z | 60.134° ENE | 20.708° | 2025-10-29 21:41:12.037Z | 21.242° NNE |
| 8 mins | 2025-10-29 23:14:12.037Z | 194.984° SSW | 2025-10-29 23:18:12.037Z | 277.554° WNW | 35.382° | 2025-10-29 23:22:12.037Z | 331.965° 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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