ARIANE 2 DEB, 27042
Orbit data source: Space-Track
ARIANE 2 DEB, 27042 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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27042 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, 0.8 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 ARIANE 2 DEB
1 27042U 89006X 26013.48232017 -.00000089 00000-0 16774-2 0 9992
2 27042 8.4600 319.8478 7139991 321.5901 301.3224 2.25354918 98017Epoch: 2026-01-13T11:34Z
TLE epoch observation values (Epoch: 2026-01-13T11:34:32.462Z)
Latitude
0.01761°
Longitude
-146.83911°
Altitude
20,986.173 km
Speed
3.593 km/s
True Right ascension
09h 19m 02s
True Declination
0° 01' 03"
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
06:36:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,751.782 km
Perigee altitude
651.735 km
Semi-major axis
24,579.896 km
Eccentricity
0.714
Inclination
8.46°
RAAN
319.8478°
Arg. of periapsis
321.5901°
True anomaly
218.41879°
Mean anomaly
301.3224°
Eccentric anomaly
260.9253°
Mean motion
0.56321 °/min
Orbital period
639.19 mins
BSTAR
0.0016774
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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. |
|---|---|---|---|---|---|---|---|
| 241 mins | 2026-01-14 06:02:23.355Z | 164.899° S | 2026-01-14 06:07:23.355Z | 165.86° S | 36.495° | 2026-01-14 10:03:23.355Z | 148.793° SSE |
| 24 mins | 2026-01-14 21:35:23.355Z | 144.292° SSE | 2026-01-14 21:42:23.355Z | 127.641° SE | 11.939° | 2026-01-14 21:59:23.355Z | 109.657° ESE |
| 361 mins | 2026-01-15 00:01:23.355Z | 97.773° ESE | 2026-01-15 04:58:23.355Z | 126.223° SE | 26.084° | 2026-01-15 06:02:23.355Z | 129.496° 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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