ARIANE 2 DEB, 42485
Orbit data source: Space-Track
ARIANE 2 DEB, 42485 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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42485 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
FRRelated business
Manufacturer
EADS/LV
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.3 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 ARIANE 2 DEB
1 42485U 89006CM 25347.88374235 -.00000008 00000-0 00000-0 0 9996
2 42485 8.4811 97.6639 6694349 67.8462 4.4747 2.17667226 94537Epoch: 2025-12-13T21:12Z
TLE epoch observation values (Epoch: 2025-12-13T21:12:35.339Z)
Latitude
8.43453°
Longitude
153.97709°
Altitude
2,409.157 km
Speed
8.653 km/s
True Right ascension
12h 59m 42s
True Declination
8° 23' 39"
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
03:10:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,615.252 km
Perigee altitude
1,936.981 km
Semi-major axis
25,154.254 km
Eccentricity
0.66943
Inclination
8.4811°
RAAN
97.6639°
Arg. of periapsis
67.8462°
True anomaly
29.35412°
Mean anomaly
4.4747°
Eccentric anomaly
13.29553°
Mean motion
0.54403 °/min
Orbital period
661.72 mins
BSTAR
0
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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 forecast
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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. |
|---|---|---|---|---|---|---|---|
| 33 mins | 2025-12-16 15:22:46.909Z | 203.252° SW | 2025-12-16 15:31:46.909Z | 160.848° S | 18.52° | 2025-12-16 15:55:46.909Z | 121.735° SE |
| 280 mins | 2025-12-16 20:14:46.909Z | 118.064° SE | 2025-12-16 23:19:46.909Z | 132.247° SE | 17.72° | 2025-12-17 00:54:46.909Z | 126.266° SE |
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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