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: 1 day ago
TLE from 1 day ago
0 METEOR 3M
1 27001U 01056A 25260.02632694 -.00000007 00000-0 45490-4 0 9993
2 27001 99.8170 76.5139 0013704 172.5173 298.9414 13.69020865187506Epoch: 2025-09-17T00:37Z
TLE epoch observation values (Epoch: 2025-09-17T00:37:54.647Z)
Latitude
66.70777°
Longitude
-85.60301°
Altitude
1,009.657 km
Speed
7.355 km/s
True Right ascension
18h 40m 19s
True Declination
66° 35' 13"
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
18:32:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,010.482 km
Perigee altitude
990.259 km
Semi-major axis
7,378.507 km
Eccentricity
0.00137
Inclination
99.817°
RAAN
76.5139°
Arg. of periapsis
172.5173°
True anomaly
298.80386°
Mean anomaly
298.9414°
Eccentric anomaly
298.87264°
Mean motion
3.42445 °/min
Orbital period
105.13 mins
BSTAR
0.00004549
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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 | 2025-09-18 11:16:54.753Z | 145.515° SSE | 2025-09-18 11:22:54.753Z | 52.719° ENE | 39.75° | 2025-09-18 11:27:54.753Z | 354.77° N |
| 8 mins | 2025-09-18 13:02:54.753Z | 225.174° WSW | 2025-09-18 13:06:54.753Z | 271.656° WNW | 20.44° | 2025-09-18 13:10:54.753Z | 313.397° NW |
| 9 mins | 2025-09-19 00:03:54.753Z | 38.836° NE | 2025-09-19 00:07:54.753Z | 94.136° ESE | 31.787° | 2025-09-19 00:12:54.753Z | 161.783° S |
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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