ARIANE 2 DEB, 27593
Orbit data source: Space-Track
ARIANE 2 DEB, 27593 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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27593 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
TLE from 15 hours ago
0 ARIANE 2 DEB
1 27593U 88040C 25213.73751039 -.00000141 00000-0 39533-3 0 9997
2 27593 7.3751 112.1874 7167794 212.7575 69.2340 2.29526603192488
Epoch: 2025-08-01T17:42Z
TLE epoch observation values (Epoch: 2025-08-01T17:42:00.897Z)
Latitude
0.00007°
Longitude
-103.8373°
Altitude
23,376.285 km
Speed
3.221 km/s
True Right ascension
07h 29m 00s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
4.85201°
Longitude
-63.28617°
Altitude
34,326.32 km
Speed
1.779 km/s
Apparent Right ascension
10h 10m 25s
Apparent Declination
0° 47' 46"
Sunlit
Visualization observer readout
Local Sidereal Time
22:03:59
Azimuth
357.453° N
Elevation
-50.853°
Doppler factor
1
Orbital elements
Apogee altitude
35,307.644 km
Perigee altitude
498.851 km
Semi-major axis
24,281.385 km
Eccentricity
0.71678
Inclination
7.3751°
RAAN
112.1874°
Arg. of periapsis
212.7575°
True anomaly
147.25389°
Mean anomaly
69.234°
Eccentric anomaly
108.2391°
Mean motion
0.57363 °/min
Orbital period
627.58 mins
BSTAR
0.00039533
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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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567 mins | 2025-08-02 13:03:43.922Z | 160.45° S | 2025-08-02 20:34:43.922Z | 152.731° SSE | 35.666° | 2025-08-02 22:30:43.922Z | 119.249° 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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