THOR ABLE DEB (YO), 115

Orbit data source: Space-Track

THOR ABLE DEB (YO), 115 is space debris in LEO originally from a launch on Fri, 01 Apr 1960 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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Identifier
115, 1960-002D
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
RCA/East Windsor
Mission
Spacecraft
Bus & Motor
Unknown
Mass
~1 kg wet, ~1 kg dry
Launch date (UTC)
1960-04-01 (65 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 THOR ABLE DEB (YO)
1 00115U 60002D   25260.34436488  .00002504  00000-0  24272-3 0  9991
2 00115  48.1647   0.9956 0026414 110.7834 249.5916 14.95719987477250
Epoch: 2025-09-17T08:15Z
TLE epoch observation values (Epoch: 2025-09-17T08:15:53.125Z)
Latitude
-0.00009°
Longitude
-119.49749°
Altitude
586.937 km
Speed
7.565 km/s
True Right ascension
00h 03m 58s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
03:38:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
599.585 km
Perigee altitude
562.82 km
Semi-major axis
6,959.339 km
Eccentricity
0.00264
Inclination
48.1647°
RAAN
0.9956°
Arg. of periapsis
110.7834°
True anomaly
249.30824°
Mean anomaly
249.5916°
Eccentric anomaly
249.44989°
Mean motion
3.73845 °/min
Orbital period
96.3 mins
BSTAR
0.00024272
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Other satellites on launch #2 in the year 1960 (1960-04-01 UTC)

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