ARIANE 4O DEB, 60247 (Decayed)
Orbit data source: Space-Track
ARIANE 4O DEB, 60247 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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60247 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: 11 months ago
TLE from 11 months ago
0 ARIANE 4O DEB
1 60247U 98017J 24303.02633675 .04101167 00000-0 13382+0 0 9994
2 60247 98.7677 314.1855 0021322 134.8763 225.4208 15.27495497 27380Epoch: 2024-10-29T00:37Z
TLE epoch observation values (Epoch: 2024-10-29T00:37:55.495Z)
Latitude
-0°
Longitude
-93.13982°
Altitude
496.647 km
Speed
7.611 km/s
True Right ascension
20h 56m 44s
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
494.945 km
Perigee altitude
465.698 km
Semi-major axis
6,858.459 km
Eccentricity
0.00213
Inclination
98.7677°
RAAN
314.1855°
Arg. of periapsis
134.8763°
True anomaly
225.24709°
Mean anomaly
225.4208°
Eccentric anomaly
225.33391°
Mean motion
3.82123 °/min
Orbital period
94.21 mins
BSTAR
0.13382
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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
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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