THOR ABLESTAR DEB, 18908 (Decayed)
Orbit data source: Space-Track
THOR ABLESTAR DEB, 18908 was space debris in LEO originally from a launch on Thu, 29 Jun 1961 UTC launched from the Air Force Eastern Test Range (AFETR). 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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18908 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 THOR ABLESTAR DEB
1 18908U 61015LY 26046.25511023 .05622898 73638-1 86935-2 0 9997
2 18908 65.6495 99.7455 0012847 4.1032 356.0249 16.08863851 22171Epoch: 2026-02-15T06:07Z
TLE epoch observation values (Epoch: 2026-02-15T06:07:21.523Z)
Latitude
-0.00005°
Longitude
-137.36064°
Altitude
243.655 km
Speed
7.766 km/s
True Right ascension
06h 38m 58s
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
15:24:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
256.851 km
Perigee altitude
239.825 km
Semi-major axis
6,626.475 km
Eccentricity
0.00128
Inclination
65.6495°
RAAN
99.7455°
Arg. of periapsis
4.1032°
True anomaly
356.01468°
Mean anomaly
356.0249°
Eccentric anomaly
356.01979°
Mean motion
4.02364 °/min
Orbital period
89.47 mins
BSTAR
0.0086935
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Other satellites on launch #15 in the year 1961 (1961-06-29 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.THOR ABLESTAR 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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