ARIANE 2 DEB, 27029
Orbit data source: Space-Track
ARIANE 2 DEB, 27029 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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27029 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
TLE from 7 months ago
0 ARIANE 2 DEB
1 27029U 89006J 25001.52767253 .00001987 00000-0 28602-1 0 9992
2 27029 8.9687 7.4621 7131308 217.5883 60.6819 2.28598028195365
Epoch: 2025-01-01T12:39Z
TLE epoch observation values (Epoch: 2025-01-01T12:39:50.906Z)
Latitude
-0°
Longitude
76.1946°
Altitude
21,155.994 km
Speed
3.546 km/s
True Right ascension
00h 30m 18s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
-2.88142°
Longitude
-163.65441°
Altitude
34,713.417 km
Speed
1.728 km/s
Apparent Right ascension
08h 39m 41s
Apparent Declination
-7° 39' 13"
Sunlit
Visualization observer readout
Local Sidereal Time
21:54:31
Azimuth
32.441° NE
Elevation
-53.652°
Doppler factor
1
Orbital elements
Apogee altitude
35,331.326 km
Perigee altitude
606.245 km
Semi-major axis
24,346.923 km
Eccentricity
0.71313
Inclination
8.9687°
RAAN
7.4621°
Arg. of periapsis
217.5883°
True anomaly
142.60474°
Mean anomaly
60.6819°
Eccentric anomaly
100.81548°
Mean motion
0.57132 °/min
Orbital period
630.12 mins
BSTAR
0.028602
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Other satellites on launch #6 in the year 1989 (1989-01-27 UTC)
ARIANE 2 DEB Visibility forecast
Observer location: undefined°, undefined°
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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575 mins | 2025-08-02 13:02:17.502Z | 226.511° WSW | 2025-08-02 17:40:17.502Z | 167.328° S | 33.295° | 2025-08-02 22:37:17.502Z | 157.603° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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