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: 8 hours ago
TLE from 8 hours ago
0 METEOR M2
1 40069U 14037A 25325.13733140 .00000160 00000-0 92481-4 0 9998
2 40069 98.4878 303.5525 0004647 285.1759 74.8904 14.21374473589769Epoch: 2025-11-21T03:17Z
TLE epoch observation values (Epoch: 2025-11-21T03:17:45.432Z)
Latitude
-0.00013°
Longitude
-166.27146°
Altitude
822.761 km
Speed
7.442 km/s
True Right ascension
20h 14m 12s
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
08:38:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
821.198 km
Perigee altitude
814.51 km
Semi-major axis
7,195.991 km
Eccentricity
0.00046
Inclination
98.4878°
RAAN
303.5525°
Arg. of periapsis
285.1759°
True anomaly
74.94182°
Mean anomaly
74.8904°
Eccentric anomaly
74.91611°
Mean motion
3.55555 °/min
Orbital period
101.25 mins
BSTAR
0.000092481
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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 | 2025-11-21 12:18:51.776Z | 354.512° N | 2025-11-21 12:22:51.776Z | 300.023° NW | 31.474° | 2025-11-21 12:27:51.776Z | 225.452° WSW |
| 7 mins | 2025-11-21 22:01:51.776Z | 124.612° SE | 2025-11-21 22:04:51.776Z | 67.681° E | 32.489° | 2025-11-21 22:08:51.776Z | 6.323° NNE |
| 7 mins | 2025-11-21 23:41:51.776Z | 220.337° SW | 2025-11-21 23:44:51.776Z | 263.031° W | 23.017° | 2025-11-21 23:48:51.776Z | 316.792° NNW |
| 4 mins | 2025-11-22 10:20:51.776Z | 73.087° E | 2025-11-22 10:21:51.776Z | 86.227° E | 16.128° | 2025-11-22 10:24:51.776Z | 123.962° SE |
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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