THOR ABLESTAR DEB, 155
Orbit data source: Space-Track
THOR ABLESTAR DEB, 155 is 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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155 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 THOR ABLESTAR DEB
1 00155U 61015AR 25314.94225976 .00004434 00000-0 11387-2 0 9990
2 00155 66.8749 132.7755 0031978 64.1607 296.2795 14.50801919329434Epoch: 2025-11-10T22:36Z
TLE epoch observation values (Epoch: 2025-11-10T22:36:51.243Z)
Latitude
-0.00003°
Longitude
103.22604°
Altitude
715.175 km
Speed
7.504 km/s
True Right ascension
08h 51m 06s
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
03:41:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
744.072 km
Perigee altitude
698.666 km
Semi-major axis
7,099.506 km
Eccentricity
0.0032
Inclination
66.8749°
RAAN
132.7755°
Arg. of periapsis
64.1607°
True anomaly
295.95035°
Mean anomaly
296.2795°
Eccentric anomaly
296.11498°
Mean motion
3.62828 °/min
Orbital period
99.22 mins
BSTAR
0.0011387
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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 forecast
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-11-11 13:37:38.145Z | 205.851° SW | 2025-11-11 13:42:38.145Z | 46.708° ENE | 44.459° | 2025-11-11 13:46:38.145Z | 29.819° NE |
| 8 mins | 2025-11-11 22:19:38.145Z | 347.13° N | 2025-11-11 22:22:38.145Z | 38.548° NE | 36.838° | 2025-11-11 22:27:38.145Z | 131.926° SE |
| 5 mins | 2025-11-12 00:02:38.145Z | 282.231° WNW | 2025-11-12 00:04:38.145Z | 252.82° W | 18.13° | 2025-11-12 00:07:38.145Z | 212.911° SW |
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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