METEOR 3M, 27001
Orbit data source: Space-Track
METEOR 3M, 27001 is a Commonwealth of Independent States-origin payload satellite in SSO that was launched on Mon, 10 Dec 2001 UTC via a ZENIT-2 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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27001 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
VNIIEM
Mission
Civil Weather
Bus & Motor
METEOR-3, Unknown motor
Mass
2,476 kg wet, ~2,300 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: 21 hours ago
TLE from 21 hours ago
0 METEOR 3M
1 27001U 01056A 25261.04902209 -.00000007 00000-0 46357-4 0 9991
2 27001 99.8170 77.5548 0013738 169.9414 299.2335 13.69020923187642Epoch: 2025-09-18T01:10Z
TLE epoch observation values (Epoch: 2025-09-18T01:10:35.508Z)
Latitude
68.74415°
Longitude
-91.04443°
Altitude
1,009.959 km
Speed
7.355 km/s
True Right ascension
18h 55m 16s
True Declination
68° 37' 54"
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
14:41:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,010.507 km
Perigee altitude
990.234 km
Semi-major axis
7,378.507 km
Eccentricity
0.00137
Inclination
99.817°
RAAN
77.5548°
Arg. of periapsis
169.9414°
True anomaly
299.09601°
Mean anomaly
299.2335°
Eccentric anomaly
299.16477°
Mean motion
3.42445 °/min
Orbital period
105.13 mins
BSTAR
0.000046357
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Other satellites on launch #56 in the year 2001 (2001-12-10 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 3M 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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-09-19 00:02:27.423Z | 31.232° NE | 2025-09-19 00:08:27.423Z | 106.297° ESE | 31.672° | 2025-09-19 00:13:27.423Z | 164.442° S |
| 9 mins | 2025-09-19 01:47:27.423Z | 350.227° N | 2025-09-19 01:51:27.423Z | 299.508° NW | 28.831° | 2025-09-19 01:56:27.423Z | 236.732° WSW |
| 5 mins | 2025-09-19 10:10:27.423Z | 78.797° E | 2025-09-19 10:12:27.423Z | 56.379° ENE | 16.454° | 2025-09-19 10:15:27.423Z | 25.14° NE |
| 11 mins | 2025-09-19 11:50:27.423Z | 168.463° S | 2025-09-19 11:55:27.423Z | 282.08° WNW | 44.57° | 2025-09-19 12:01:27.423Z | 343.111° N |
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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