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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METEOR M2 radio frequencies
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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: 13 hours ago
TLE from 13 hours ago
0 METEOR M2
1 40069U 14037A 25255.58658549 .00000090 00000-0 60364-4 0 9995
2 40069 98.4777 236.7128 0006785 117.3359 242.8510 14.21330757579889Epoch: 2025-09-12T14:04Z
TLE epoch observation values (Epoch: 2025-09-12T14:04:40.986Z)
Latitude
-0.00004°
Longitude
33.70986°
Altitude
826.011 km
Speed
7.439 km/s
True Right ascension
15h 46m 51s
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
19:20:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
822.884 km
Perigee altitude
813.119 km
Semi-major axis
7,196.139 km
Eccentricity
0.00068
Inclination
98.4777°
RAAN
236.7128°
Arg. of periapsis
117.3359°
True anomaly
242.78184°
Mean anomaly
242.851°
Eccentric anomaly
242.81642°
Mean motion
3.55544 °/min
Orbital period
101.25 mins
BSTAR
0.000060364
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-09-13 10:56:29.572Z | 35.478° NE | 2025-09-13 11:00:29.572Z | 88.858° E | 28.166° | 2025-09-13 11:05:29.572Z | 159.481° S |
| 7 mins | 2025-09-13 12:37:29.572Z | 344.089° N | 2025-09-13 12:40:29.572Z | 300.286° NW | 26.747° | 2025-09-13 12:44:29.572Z | 238.864° WSW |
| 9 mins | 2025-09-13 22:18:29.572Z | 140.905° SSE | 2025-09-13 22:22:29.572Z | 72.67° E | 37.249° | 2025-09-13 22:27:29.572Z | 358.348° N |
| 6 mins | 2025-09-14 00:00:29.572Z | 234.397° WSW | 2025-09-14 00:02:29.572Z | 261.158° W | 18.68° | 2025-09-14 00:06:29.572Z | 311.661° NW |
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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