ARIANE 5 R/B, 41946
Orbit data source: Space-Track
ARIANE 5 R/B, 41946 is space debris in HEO originally from a launch on Tue, 14 Feb 2017 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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41946 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 ARIANE 5 R/B
1 41946U 17007C 25243.43571784 .00002980 00000-0 12383-2 0 9992
2 41946 4.0344 48.8018 7182258 289.5971 10.1892 2.39621788 72437
Epoch: 2025-08-31T10:27Z
TLE epoch observation values (Epoch: 2025-08-31T10:27:26.021Z)
Latitude
0.00001°
Longitude
-87.51237°
Altitude
2,835.864 km
Speed
8.343 km/s
True Right ascension
03h 16m 48s
True Declination
0° 00' 00"
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
14:14:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,163.326 km
Perigee altitude
270.313 km
Semi-major axis
23,594.957 km
Eccentricity
0.71823
Inclination
4.0344°
RAAN
48.8018°
Arg. of periapsis
289.5971°
True anomaly
70.58565°
Mean anomaly
10.1892°
Eccentric anomaly
31.98995°
Mean motion
0.59884 °/min
Orbital period
601.16 mins
BSTAR
0.0012383
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Other satellites on launch #7 in the year 2017 (2017-02-14 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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342 mins | 2025-09-01 16:51:03.959Z | 237.241° WSW | 2025-09-01 18:55:03.959Z | 215.662° SW | 33.027° | 2025-09-01 22:33:03.959Z | 238.931° WSW |
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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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