ARIANE 5 R/B, 41383
Orbit data source: Space-Track
ARIANE 5 R/B, 41383 is space debris in HEO originally from a launch on Wed, 09 Mar 2016 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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41383 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
TLE from 19 hours ago
0 ARIANE 5 R/B
1 41383U 16014B 25199.17871808 .00005307 00000-0 64629-3 0 9992
2 41383 0.3398 185.6434 6577483 17.4968 103.3503 3.23037299 91733
Epoch: 2025-07-18T04:17Z
TLE epoch observation values (Epoch: 2025-07-18T04:17:21.242Z)
Latitude
0.02394°
Longitude
-0.57241°
Altitude
21,371.026 km
Speed
2.848 km/s
True Right ascension
23h 59m 59s
True Declination
0° 01' 26"
Sunlit
Visualization orbit readout
Latitude
-0.31649°
Longitude
84.36438°
Altitude
9,671.899 km
Speed
5.389 km/s
Apparent Right ascension
04h 36m 51s
Apparent Declination
-13° 13' 17"
Sunlit
Visualization observer readout
Local Sidereal Time
12:26:26
Azimuth
277.383° WNW
Elevation
-29.361°
Doppler factor
1
Orbital elements
Apogee altitude
25,675.11 km
Perigee altitude
239.441 km
Semi-major axis
19,335.413 km
Eccentricity
0.65775
Inclination
0.3398°
RAAN
185.6434°
Arg. of periapsis
17.4968°
True anomaly
156.89249°
Mean anomaly
103.3503°
Eccentric anomaly
131.55264°
Mean motion
0.80726 °/min
Orbital period
445.95 mins
BSTAR
0.00064629
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Other satellites on launch #14 in the year 2016 (2016-03-09 UTC)
ARIANE 5 R/B 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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379 mins | 2025-07-19 08:17:47.599Z | 213.66° SW | 2025-07-19 12:01:47.599Z | 154.533° SSE | 31.572° | 2025-07-19 14:36:47.599Z | 127.717° SE |
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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