METEOSAT 2, 12544
Orbit data source: Space-Track
METEOSAT 2, 12544 is a payload satellite owned by ESA (ESA) in GEO that was launched on Fri, 19 Jun 1981 UTC via an ARIANE 1 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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12544 intel report (Beta)
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Identifier
Orbit
Country
ESARelated business
Manufacturer
Ae/Cannes
Mission
Non-operational spacecraft
Bus & Motor
METEOSAT, MAGE 1
Mass
324 kg wet, 282 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 METEOSAT 2
1 12544U 81057A 26064.67420844 -.00000078 00000-0 00000-0 0 9996
2 12544 10.4456 320.0018 0030814 13.1841 173.6961 0.98723048122825Epoch: 2026-03-05T16:10Z
TLE epoch observation values (Epoch: 2026-03-05T16:10:51.609Z)
Latitude
-1.2574°
Longitude
100.72406°
Altitude
36,357.255 km
Speed
3.049 km/s
True Right ascension
09h 47m 26s
True Declination
-1° 15' 22"
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
10:50:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,358.722 km
Perigee altitude
36,096.152 km
Semi-major axis
42,605.574 km
Eccentricity
0.00308
Inclination
10.4456°
RAAN
320.0018°
Arg. of periapsis
13.1841°
True anomaly
173.73472°
Mean anomaly
173.6961°
Eccentric anomaly
173.71543°
Mean motion
0.2468 °/min
Orbital period
1,458.68 mins
BSTAR
0
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Other satellites on launch #57 in the year 1981 (1981-06-19 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 2 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 2 is likely not visible in the next few days. |
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12544 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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