ARIANE 5 R/B, 28913
Orbit data source: Space-Track
ARIANE 5 R/B, 28913 is space debris in HEO originally from a launch on Wed, 21 Dec 2005 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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28913 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
TLE from 14 hours ago
0 ARIANE 5 R/B
1 28913U 05049C 25206.47245154 -.00000096 00000-0 20437-2 0 9992
2 28913 4.0598 70.6560 7138535 101.5224 143.4758 2.24894156161036
Epoch: 2025-07-25T11:20Z
TLE epoch observation values (Epoch: 2025-07-25T11:20:19.813Z)
Latitude
-4.06724°
Longitude
-130.24921°
Altitude
34,580.413 km
Speed
1.807 km/s
True Right ascension
22h 53m 01s
True Declination
-4° 03' 47"
Sunlit
Visualization orbit readout
Latitude
-3.39706°
Longitude
-99.57393°
Altitude
29,519.985 km
Speed
2.451 km/s
Apparent Right ascension
01h 08m 34s
Apparent Declination
-8° 45' 04"
Sunlit
Visualization observer readout
Local Sidereal Time
14:45:21
Azimuth
41.259° NE
Elevation
-52.1°
Doppler factor
1
Orbital elements
Apogee altitude
35,805.916 km
Perigee altitude
664.95 km
Semi-major axis
24,613.57 km
Eccentricity
0.71385
Inclination
4.0598°
RAAN
70.656°
Arg. of periapsis
101.5224°
True anomaly
171.11953°
Mean anomaly
143.4758°
Eccentric anomaly
158.47956°
Mean motion
0.56206 °/min
Orbital period
640.5 mins
BSTAR
0.0020437
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Other satellites on launch #49 in the year 2005 (2005-12-21 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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592 mins | 2025-07-26 04:47:49.062Z | 208.339° SW | 2025-07-26 10:38:49.062Z | 178.913° S | 32.411° | 2025-07-26 14:39:49.062Z | 140.778° 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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