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: 1 day ago

TLE from 1 day ago
0 THOR ABLE DEB (YO)
1   115U 60002D   26047.16553531  .00003792  00000-0  34184-3 0  9997
2   115  48.1640 335.9356 0026569  72.4438 287.9380 14.97321757499995
Epoch: 2026-02-16T03:58Z
TLE epoch observation values (Epoch: 2026-02-16T03:58:22.250Z)
Latitude
-0.00003°
Longitude
130.17907°
Altitude
569.878 km
Speed
7.581 km/s
True Right ascension
22h 23m 44s
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
17:01:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
594.717 km
Perigee altitude
557.763 km
Semi-major axis
6,954.377 km
Eccentricity
0.00266
Inclination
48.164°
RAAN
335.9356°
Arg. of periapsis
72.4438°
True anomaly
287.64805°
Mean anomaly
287.938°
Eccentric anomaly
287.79305°
Mean motion
3.74245 °/min
Orbital period
96.19 mins
BSTAR
0.00034184
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Other satellites on launch #2 in the year 1960 (1960-04-01 UTC)

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