ARIANE 5 DEB (SYLDA), 43635 (Decayed)
Orbit data source: Space-Track
ARIANE 5 DEB (SYLDA), 43635 was space debris in LEO originally from a launch on Tue, 25 Sep 2018 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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43635 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
FRRelated business
Manufacturer
ADS/Bremen
Mission
Decayed spacecraft
Bus & Motor
SYLDA 5, Unknown motor
Mass
440 kg wet, 440 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 2.8 m
Radar Cross Section
27.391 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 months ago
TLE from 8 months ago
0 ARIANE 5 DEB (SYLDA)
1 43635U 18074D 24356.22750071 .07451130 -20805-4 53576-2 0 9994
2 43635 6.1947 224.4420 1064540 37.5189 93.6934 13.87638991 78443Epoch: 2024-12-21T05:27Z
TLE epoch observation values (Epoch: 2024-12-21T05:27:36.061Z)
Latitude
3.72472°
Longitude
-164.37461°
Altitude
1,064.763 km
Speed
7.257 km/s
True Right ascension
00h 31m 13s
True Declination
3° 42' 12"
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
13:55:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,722.3 km
Perigee altitude
163.584 km
Semi-major axis
7,321.079 km
Eccentricity
0.10645
Inclination
6.1947°
RAAN
224.442°
Arg. of periapsis
37.5189°
True anomaly
105.67549°
Mean anomaly
93.6934°
Eccentric anomaly
99.70547°
Mean motion
3.46482 °/min
Orbital period
103.9 mins
BSTAR
0.0053576
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Other satellites on launch #74 in the year 2018 (2018-09-25 UTC)
ARIANE 5 DEB (SYLDA) Visibility
Observer location: undefined°, undefined°
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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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Authenticating...
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