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: 23 hours ago

TLE from 23 hours ago
0 THOR ABLE DEB (YO)
1   115U 60002D   26038.29018860  .00004742  00000-0  42273-3 0  9996
2   115  48.1635  19.5385 0026876  31.5369 328.7154 14.97252259498662
Epoch: 2026-02-07T06:57Z
TLE epoch observation values (Epoch: 2026-02-07T06:57:52.295Z)
Latitude
0.00003°
Longitude
137.65479°
Altitude
559.781 km
Speed
7.592 km/s
True Right ascension
01h 18m 09s
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
07:59:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
595.146 km
Perigee altitude
557.764 km
Semi-major axis
6,954.592 km
Eccentricity
0.00269
Inclination
48.1635°
RAAN
19.5385°
Arg. of periapsis
31.5369°
True anomaly
328.55501°
Mean anomaly
328.7154°
Eccentric anomaly
328.63525°
Mean motion
3.74227 °/min
Orbital period
96.2 mins
BSTAR
0.00042273
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Other satellites on launch #2 in the year 1960 (1960-04-01 UTC)

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