ARIANE 5 DEB, 43384
Orbit data source: Space-Track
ARIANE 5 DEB, 43384 is space debris in HEO originally from a launch on Thu, 12 Jun 2008 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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43384 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
TLE from 1 day ago
0 ARIANE 5 DEB
1 43384U 08030G 25198.92134909 .00000149 00000-0 46266-3 0 9996
2 43384 1.9797 43.8195 7186545 171.6674 214.2782 2.30541341138488
Epoch: 2025-07-17T22:06Z
TLE epoch observation values (Epoch: 2025-07-17T22:06:44.561Z)
Latitude
0.00011°
Longitude
136.05836°
Altitude
34,140.565 km
Speed
1.791 km/s
True Right ascension
02h 54m 53s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
-2.02128°
Longitude
47.73556°
Altitude
6,920.515 km
Speed
6.593 km/s
Apparent Right ascension
21h 54m 54s
Apparent Declination
-15° 09' 20"
Sunlit
Visualization observer readout
Local Sidereal Time
12:29:44
Azimuth
64.896° ENE
Elevation
-48.199°
Doppler factor
1
Orbital elements
Apogee altitude
35,230.971 km
Perigee altitude
433.317 km
Semi-major axis
24,210.281 km
Eccentricity
0.71865
Inclination
1.9797°
RAAN
43.8195°
Arg. of periapsis
171.6674°
True anomaly
188.20973°
Mean anomaly
214.2782°
Eccentric anomaly
200.11655°
Mean motion
0.57616 °/min
Orbital period
624.83 mins
BSTAR
0.00046266
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Other satellites on launch #30 in the year 2008 (2008-06-12 UTC)
ARIANE 5 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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573 mins | 2025-07-19 10:05:04.966Z | 220.967° SW | 2025-07-19 13:16:04.966Z | 192.216° SSW | 33.678° | 2025-07-19 19:38:04.966Z | 160.032° 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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