ARIANE 4O DEB, 60248 (Decayed)
Orbit data source: Space-Track
ARIANE 4O DEB, 60248 was space debris in SSO originally from a launch on Tue, 24 Mar 1998 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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60248 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
FRRelated business
Manufacturer
Unknown
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 9 months ago
TLE from 9 months ago
0 ARIANE 4O DEB
1 60248U 98017K 24355.78274301 .00132179 00000-0 20753-1 0 9997
2 60248 98.8387 8.5995 0019251 251.5365 108.3747 14.71688573 34946Epoch: 2024-12-20T18:47Z
TLE epoch observation values (Epoch: 2024-12-20T18:47:08.996Z)
Latitude
-0.00001°
Longitude
-3.03129°
Altitude
662.956 km
Speed
7.523 km/s
True Right ascension
00h 34m 23s
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
18:29:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
666.314 km
Perigee altitude
639.244 km
Semi-major axis
7,030.916 km
Eccentricity
0.00193
Inclination
98.8387°
RAAN
8.5995°
Arg. of periapsis
251.5365°
True anomaly
108.58389°
Mean anomaly
108.3747°
Eccentric anomaly
108.47931°
Mean motion
3.6815 °/min
Orbital period
97.79 mins
BSTAR
0.020753
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Other satellites on launch #17 in the year 1998 (1998-03-24 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ARIANE 4O DEB Visibility
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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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| This satellite is decayed. |
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
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