METEOSAT 3 AKM, 43333
Orbit data source: Space-Track
METEOSAT 3 AKM, 43333 is space debris in GEO originally from a launch on Wed, 15 Jun 1988 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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43333 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 METEOSAT 3 AKM
1 43333U 88051G 25242.31388423 .00000060 00000-0 00000-0 0 9991
2 43333 12.3204 332.0759 0059461 169.1647 191.0134 0.99532875 42809
Epoch: 2025-08-30T07:31Z
TLE epoch observation values (Epoch: 2025-08-30T07:31:59.597Z)
Latitude
0.00001°
Longitude
-119.63533°
Altitude
36,242.963 km
Speed
3.049 km/s
True Right ascension
22h 08m 27s
True Declination
0° 00' 00"
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
06:10:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,247.974 km
Perigee altitude
35,744.052 km
Semi-major axis
42,374.15 km
Eccentricity
0.00595
Inclination
12.3204°
RAAN
332.0759°
Arg. of periapsis
169.1647°
True anomaly
190.88417°
Mean anomaly
191.0134°
Eccentric anomaly
190.94869°
Mean motion
0.24882 °/min
Orbital period
1,446.81 mins
BSTAR
0
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Other satellites on launch #51 in the year 1988 (1988-06-15 UTC)
METEOSAT 3 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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1440 mins | 2025-08-31 14:30:47.825Z | 214.98° SW | 2025-08-31 14:30:47.825Z | 214.98° SW | 38.459° | 2025-09-01 14:30:47.825Z | 219.351° SW |
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43333 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
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