METEOSAT 5 AKM, 21904
Orbit data source: Space-Track
METEOSAT 5 AKM, 21904 is space debris in GEO originally from a launch on Sat, 02 Mar 1991 UTC launched from the French Guiana (FRGUI). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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21904 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
1 day ago
Origin
Manufacturer
SEP
Mission
Spacecraft
Bus & Motor
MAGE, Unknown motor
Mass
358 kg wet, 70 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl + Cone, 1.12 m
Radar Cross Section
0.910 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & history
TLE from 1 day ago
0 METEOSAT 5 AKM
1 21904U 91015E 25108.08513286 -.00000357 00000-0 00000+0 0 9996
2 21904 12.6349 341.1296 0155115 225.7487 132.9146 1.00124123112231Epoch: 2025-04-18T02:02Z
Definitive object data (Epoch: 2025-04-18T02:02:35.479Z)
Latitude
0.00001°
Longitude
103.98933°
Altitude
36,280.737 km
Speed
3.04 km/s
True Right ascension
22h 44m 20s
True Declination
0° 00' 00"
Sunlit
Visualization TLE readout
Latitude
2.79245°
Longitude
-88.57616°
Altitude
35,478.52 km
Speed
3.099 km/s
Apparent Right ascension
09h 43m 30s
Apparent Declination
-2° 31' 01"
Sunlit
Visualization observer readout
Local Sidereal Time
20:10:47
Azimuth
324.712° NNW
Elevation
-47.102°
Doppler factor
1
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21904 neighbors
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Other satellites on launch #15 in the year 1991 (1991-03-02 UTC)
METEOSAT 5 AKM Visibility forecast
Observer location: undefined°, undefined°
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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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