ARIANE 2 DEB, 40787
Orbit data source: Space-Track
ARIANE 2 DEB, 40787 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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40787 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, 1.1 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 40787U 89006CG 25331.83614625 -.00000056 00000-0 52628-3 0 9996
2 40787 8.4983 323.9796 7140019 314.0263 179.7223 2.25290078 98902Epoch: 2025-11-27T20:04Z
TLE epoch observation values (Epoch: 2025-11-27T20:04:03.036Z)
Latitude
6.11653°
Longitude
90.21221°
Altitude
35,753.355 km
Speed
1.645 km/s
True Right ascension
06h 32m 50s
True Declination
6° 06' 37"
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
05:47:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,759.928 km
Perigee altitude
653.014 km
Semi-major axis
24,584.608 km
Eccentricity
0.714
Inclination
8.4983°
RAAN
323.9796°
Arg. of periapsis
314.0263°
True anomaly
179.93382°
Mean anomaly
179.7223°
Eccentric anomaly
179.83798°
Mean motion
0.56305 °/min
Orbital period
639.37 mins
BSTAR
0.00052628
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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. |
|---|---|---|---|---|---|---|---|
| 18 mins | 2025-11-29 11:44:45.936Z | 262.682° W | 2025-11-29 11:54:45.936Z | 262.813° W | 10.068° | 2025-11-29 12:02:45.936Z | 262.982° W |
| 53 mins | 2025-11-30 07:20:45.936Z | 247.197° WSW | 2025-11-30 08:13:45.936Z | 229.533° WSW | 30.964° | 2025-11-30 08:13:45.936Z | 229.533° WSW |
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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