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: 3 days ago

TLE from 3 days ago
0 THOR ABLE DEB (YO)
1 00115U 60002D   25317.71353479  .00010389  00000-0  91868-3 0  9998
2 00115  48.1624  79.6731 0026929   5.4319 354.6886 14.96424525485848
Epoch: 2025-11-13T17:07Z
TLE epoch observation values (Epoch: 2025-11-13T17:07:29.405Z)
Latitude
-0.00005°
Longitude
129.73311°
Altitude
559.651 km
Speed
7.593 km/s
True Right ascension
05h 18m 41s
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
08:13:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
597.754 km
Perigee altitude
560.284 km
Semi-major axis
6,957.156 km
Eccentricity
0.00269
Inclination
48.1624°
RAAN
79.6731°
Arg. of periapsis
5.4319°
True anomaly
354.65994°
Mean anomaly
354.6886°
Eccentric anomaly
354.67428°
Mean motion
3.74021 °/min
Orbital period
96.25 mins
BSTAR
0.00091868
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Other satellites on launch #2 in the year 1960 (1960-04-01 UTC)

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