ARIANE 2 DEB, 28562
Orbit data source: Space-Track
ARIANE 2 DEB, 28562 is space debris in HEO originally from a launch on Tue, 17 May 1988 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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28562 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
TLE from 5 hours ago
0 ARIANE 2 DEB
1 28562U 88040F 25214.46061738 .00000642 00000-0 32586-2 0 9990
2 28562 8.0747 342.4933 7053099 112.4198 332.7633 2.46426565195134
Epoch: 2025-08-02T11:03Z
TLE epoch observation values (Epoch: 2025-08-02T11:03:17.341Z)
Latitude
0.00001°
Longitude
-134.49977°
Altitude
9,503.973 km
Speed
5.742 km/s
True Right ascension
22h 50m 28s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
-7.68008°
Longitude
153.54755°
Altitude
32,813.909 km
Speed
1.768 km/s
Apparent Right ascension
18h 01m 49s
Apparent Declination
-12° 00' 28"
Sunlit
Visualization observer readout
Local Sidereal Time
05:55:08
Azimuth
356.511° N
Elevation
-62.053°
Doppler factor
1
Orbital elements
Apogee altitude
33,114.027 km
Perigee altitude
446.4 km
Semi-major axis
23,158.35 km
Eccentricity
0.70531
Inclination
8.0747°
RAAN
342.4933°
Arg. of periapsis
112.4198°
True anomaly
247.93173°
Mean anomaly
332.7633°
Eccentric anomaly
296.64296°
Mean motion
0.61586 °/min
Orbital period
584.55 mins
BSTAR
0.0032586
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Other satellites on launch #40 in the year 1988 (1988-05-17 UTC)
ARIANE 2 DEB 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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524 mins | 2025-08-02 21:52:35.218Z | 183.144° SSW | 2025-08-03 04:50:35.218Z | 151.711° SSE | 27.198° | 2025-08-03 06:36:35.218Z | 125.515° 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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