METEOSAT 6, 22912
Orbit data source: Space-Track
METEOSAT 6, 22912 is a payload satellite owned by EUMETSAT (DE) in GEO that was launched on Sat, 20 Nov 1993 UTC via an ARIANE 44LP launch vehicle from the French Guiana (FRGUI). 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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22912 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / EUMERelated business
Manufacturer
Ae/Cannes
Mission
Non-operational Civil Weather
Bus & Motor
METEOSAT, MAGE 1
Mass
318 kg wet, 278 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + Cyl + 1 Ant, 1.7 m
Radar Cross Section
4.680 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 METEOSAT 6
1 22912U 93073B 25360.25536170 -.00000222 00000-0 00000+0 0 9999
2 22912 14.4409 2.5490 0010047 239.1355 292.8976 0.98986375115308Epoch: 2025-12-26T06:07Z
TLE epoch observation values (Epoch: 2025-12-26T06:07:43.250Z)
Latitude
2.01302°
Longitude
-12.20519°
Altitude
36,133.717 km
Speed
3.063 km/s
True Right ascension
11h 38m 53s
True Declination
2° 00' 40"
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
14:18:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,194.531 km
Perigee altitude
36,109.071 km
Semi-major axis
42,529.938 km
Eccentricity
0.001
Inclination
14.4409°
RAAN
2.549°
Arg. of periapsis
239.1355°
True anomaly
292.79149°
Mean anomaly
292.8976°
Eccentric anomaly
292.84455°
Mean motion
0.24746 °/min
Orbital period
1,454.79 mins
BSTAR
0
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Other satellites on launch #73 in the year 1993 (1993-11-20 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.METEOSAT 6 Visibility
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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. |
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| METEOSAT 6 is likely not visible in the next few days. |
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22912 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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