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
3 days 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 3 days ago
0 METEOSAT 5 AKM
1 21904U 91015E 25118.07255690 -.00000339 00000-0 00000-0 0 9999
2 21904 12.6260 341.0643 0155043 225.7999 132.8352 1.00119845112217Epoch: 2025-04-28T01:44Z
Definitive object data (Epoch: 2025-04-28T01:44:28.916Z)
Latitude
-0°
Longitude
98.5869°
Altitude
36,280.889 km
Speed
3.04 km/s
True Right ascension
22h 43m 59s
True Declination
0° 00' 00"
Sunlit
Visualization TLE readout
Latitude
9.59028°
Longitude
147.49131°
Altitude
36,484.346 km
Speed
3.026 km/s
Apparent Right ascension
01h 51m 28s
Apparent Declination
3° 44' 12"
Sunlit
Visualization observer readout
Local Sidereal Time
12:40:05
Azimuth
335.122° NNW
Elevation
-43.37°
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°
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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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