ARIANE 44L+3 R/B, 23950
Orbit data source: Space-Track
ARIANE 44L+3 R/B, 23950 is space debris in HEO originally from a launch on Tue, 09 Jul 1996 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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23950 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 ARIANE 44L+3 R/B
1 23950U 96040C 25251.28565384 .00001894 00000-0 14410-2 0 9998
2 23950 7.1970 306.7869 6904146 309.9326 7.4755 2.72302099263560
Epoch: 2025-09-08T06:51Z
TLE epoch observation values (Epoch: 2025-09-08T06:51:20.491Z)
Latitude
0.00014°
Longitude
-143.55566°
Altitude
1,505.257 km
Speed
9.095 km/s
True Right ascension
20h 27m 29s
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
20:00:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
30,248.734 km
Perigee altitude
329.77 km
Semi-major axis
21,667.389 km
Eccentricity
0.69041
Inclination
7.197°
RAAN
306.7869°
Arg. of periapsis
309.9326°
True anomaly
50.48252°
Mean anomaly
7.4755°
Eccentric anomaly
22.81315°
Mean motion
0.68051 °/min
Orbital period
529.02 mins
BSTAR
0.001441
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Other satellites on launch #40 in the year 1996 (1996-07-09 UTC)
ARIANE 44L+3 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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472 mins | 2025-09-09 09:35:46.007Z | 232.362° WSW | 2025-09-09 12:03:46.007Z | 185.541° SSW | 37.215° | 2025-09-09 17:27:46.007Z | 154.695° SSE |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
Authenticating...
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