ARIANE 2 DEB, 29023
Orbit data source: Space-Track
ARIANE 2 DEB, 29023 is space debris in HEO originally from a launch on Fri, 27 Jan 1989 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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29023 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 ARIANE 2 DEB
1 29023U 89006AP 25348.64674900 -.00000564 00000-0 -26142-1 0 9990
2 29023 8.1339 49.3107 7074121 143.5383 266.5666 2.25235566 95934Epoch: 2025-12-14T15:31Z
TLE epoch observation values (Epoch: 2025-12-14T15:31:19.113Z)
Latitude
-1.76641°
Longitude
80.37099°
Altitude
28,472.41 km
Speed
2.581 km/s
True Right ascension
02h 27m 01s
True Declination
-1° 45' 51"
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
13:22:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,604.472 km
Perigee altitude
816.145 km
Semi-major axis
24,588.446 km
Eccentricity
0.70741
Inclination
8.1339°
RAAN
49.3107°
Arg. of periapsis
143.5383°
True anomaly
203.7419°
Mean anomaly
266.5666°
Eccentric anomaly
233.84169°
Mean motion
0.56292 °/min
Orbital period
639.52 mins
BSTAR
-0.026142
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Other satellites on launch #6 in the year 1989 (1989-01-27 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 2 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 2 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
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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