ARIANE 2 DEB, 42489
Orbit data source: Space-Track
ARIANE 2 DEB, 42489 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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42489 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
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 ARIANE 2 DEB
1 42489U 89006CR 24228.46125038 -.00000097 00000-0 00000+0 0 9993
2 42489 9.8006 51.3859 6820659 144.5476 85.0904 2.19970790170952Epoch: 2024-08-15T11:04Z
TLE epoch observation values (Epoch: 2024-08-15T11:04:12.032Z)
Latitude
-8.82075°
Longitude
-142.80157°
Altitude
26,925.253 km
Speed
2.824 km/s
True Right ascension
23h 10m 23s
True Declination
-8° 48' 35"
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
02:05:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,637.419 km
Perigee altitude
1,563.394 km
Semi-major axis
24,978.543 km
Eccentricity
0.68207
Inclination
9.8006°
RAAN
51.3859°
Arg. of periapsis
144.5476°
True anomaly
151.38284°
Mean anomaly
85.0904°
Eccentric anomaly
119.20282°
Mean motion
0.54978 °/min
Orbital period
654.8 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. |
|---|---|---|---|---|---|---|---|
| 487 mins | 2025-09-15 09:27:19.271Z | 110.373° ESE | 2025-09-15 15:00:19.271Z | 143.334° SSE | 26.515° | 2025-09-15 17:34:19.271Z | 137.78° SSE |
| 7 mins | 2025-09-16 05:40:19.271Z | 152.502° SSE | 2025-09-16 05:42:19.271Z | 143.149° SSE | 11.415° | 2025-09-16 05:47:19.271Z | 126.15° 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 ascending 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 ascending order |
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