ARIANE 40 DEB, 35955 (Decayed)
Orbit data source: Space-Track
ARIANE 40 DEB, 35955 was space debris in LEO originally from a launch on Sun, 26 Sep 1993 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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35955 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
FRRelated business
Manufacturer
Unknown
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 ARIANE 40 DEB
1 35955U 93061K 24205.15759195 .25593434 32983-5 68685-2 0 9991
2 35955 98.6080 30.1642 0021296 286.1507 73.7438 16.27590434781240Epoch: 2024-07-23T03:46Z
TLE epoch observation values (Epoch: 2024-07-23T03:46:55.944Z)
Latitude
-0.00002°
Longitude
32.05108°
Altitude
198.325 km
Speed
7.79 km/s
True Right ascension
02h 00m 39s
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
06:49:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
209.905 km
Perigee altitude
181.905 km
Semi-major axis
6,574.042 km
Eccentricity
0.00213
Inclination
98.608°
RAAN
30.1642°
Arg. of periapsis
286.1507°
True anomaly
73.97825°
Mean anomaly
73.7438°
Eccentric anomaly
73.86101°
Mean motion
4.07187 °/min
Orbital period
88.41 mins
BSTAR
0.0068685
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Other satellites on launch #61 in the year 1993 (1993-09-26 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ARIANE 40 DEB Visibility
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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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| This satellite is decayed. |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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