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 (66 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 18 hours ago

TLE from 18 hours ago
0 THOR ABLE DEB (YO)
1 00115U 60002D   25352.83102393  .00002713  00000-0  25438-3 0  9999
2 00115  48.1625 267.3319 0027159 166.1213 194.0457 14.96746265491105
Epoch: 2025-12-18T19:56Z
TLE epoch observation values (Epoch: 2025-12-18T19:56:40.467Z)
Latitude
-0.00003°
Longitude
-119.51763°
Altitude
595.631 km
Speed
7.554 km/s
True Right ascension
17h 49m 19s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
12:45:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
596.914 km
Perigee altitude
559.13 km
Semi-major axis
6,956.159 km
Eccentricity
0.00272
Inclination
48.1625°
RAAN
267.3319°
Arg. of periapsis
166.1213°
True anomaly
193.97042°
Mean anomaly
194.0457°
Eccentric anomaly
194.00803°
Mean motion
3.74101 °/min
Orbital period
96.23 mins
BSTAR
0.00025438
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Other satellites on launch #2 in the year 1960 (1960-04-01 UTC)

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