ARIANE 5 R/B, 45248
Orbit data source: Space-Track
ARIANE 5 R/B, 45248 is space debris in HEO originally from a launch on Tue, 18 Feb 2020 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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45248 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
TLE from 20 hours ago
0 ARIANE 5 R/B
1 45248U 20013D 25199.13793252 .00001451 00000-0 54634-3 0 9993
2 45248 5.1963 182.7177 7164806 56.0836 352.5927 2.41953536 46384
Epoch: 2025-07-18T03:18Z
TLE epoch observation values (Epoch: 2025-07-18T03:18:37.369Z)
Latitude
0.00004°
Longitude
-163.46815°
Altitude
1,799.272 km
Speed
8.97 km/s
True Right ascension
12h 09m 31s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
5.05193°
Longitude
-60.20689°
Altitude
1,257.319 km
Speed
9.348 km/s
Apparent Right ascension
21h 00m 08s
Apparent Declination
-19° 08' 51"
Sunlit
Visualization observer readout
Local Sidereal Time
12:18:43
Azimuth
78.924° E
Elevation
-42.814°
Doppler factor
1
Orbital elements
Apogee altitude
33,861.526 km
Perigee altitude
268.443 km
Semi-major axis
23,443.121 km
Eccentricity
0.71648
Inclination
5.1963°
RAAN
182.7177°
Arg. of periapsis
56.0836°
True anomaly
304.17338°
Mean anomaly
352.5927°
Eccentric anomaly
335.69854°
Mean motion
0.60467 °/min
Orbital period
595.36 mins
BSTAR
0.00054634
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Other satellites on launch #13 in the year 2020 (2020-02-18 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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543 mins | 2025-07-19 09:37:06.486Z | 208.243° SW | 2025-07-19 15:17:06.486Z | 170.364° S | 31.289° | 2025-07-19 18:40:06.486Z | 142.624° 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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