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.

Not visible in the next 10 days
Identifier
21904, 1991-015E
Orbit
GEO
Country
Flag of ESAESA
Related business
Manufacturer
SEP
Mission
Spacecraft
Bus & Motor
MAGE, Unknown motor
Mass
358 kg wet, 70 kg dry
Launch date (UTC)
1991-03-02 (35 years ago)
Launch vehicle
Unknown
Launch site
French Guiana (FRGUI)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + Cone, 0.6 m
Radar Cross Section
0.910 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 21 hours ago

TLE from 21 hours ago
0 METEOSAT 5 AKM
1 21904U 91015E   25348.74696532 -.00000208  00000-0  00000-0 0  9997
2 21904  12.4248 339.5553 0159243 233.3433 125.1586  1.00166720114521
Epoch: 2025-12-14T17:55Z
TLE epoch observation values (Epoch: 2025-12-14T17:55:37.803Z)
Latitude
-0°
Longitude
-13.0366°
Altitude
36,207.069 km
Speed
3.045 km/s
True Right ascension
22h 38m 06s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
13:22:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,489.001 km
Perigee altitude
35,145.143 km
Semi-major axis
42,195.209 km
Eccentricity
0.01592
Inclination
12.4248°
RAAN
339.5553°
Arg. of periapsis
233.3433°
True anomaly
126.6334°
Mean anomaly
125.1586°
Eccentric anomaly
125.8977°
Mean motion
0.25041 °/min
Orbital period
1,437.65 mins
BSTAR
0
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