ARIANE 1 DEB, 25767
Orbit data source: Space-Track
ARIANE 1 DEB, 25767 is space debris originally from a launch on Mon, 24 Dec 1979 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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25767 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 ARIANE 1 DEB
1 25767U 79104J 25295.42969882 .00119462 00000-0 78496-2 0 9998
2 25767 17.8056 220.3621 2516760 59.8026 322.7869 10.26617121358403
Epoch: 2025-10-22T10:18Z
TLE epoch observation values (Epoch: 2025-10-22T10:18:45.978Z)
Latitude
0.00001°
Longitude
34.56714°
Altitude
1,054.077 km
Speed
7.919 km/s
True Right ascension
14h 41m 26s
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
18:02:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
4,820.931 km
Perigee altitude
317.311 km
Semi-major axis
8,947.258 km
Eccentricity
0.25168
Inclination
17.8056°
RAAN
220.3621°
Arg. of periapsis
59.8026°
True anomaly
300.23096°
Mean anomaly
322.7869°
Eccentric anomaly
312.08512°
Mean motion
2.56453 °/min
Orbital period
140.38 mins
BSTAR
0.0078496
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Other satellites on launch #104 in the year 1979 (1979-12-24 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 1 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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ARIANE 1 DEB is likely not visible in the next few days. |
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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