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: 10 hours ago

TLE from 10 hours ago
0 THOR ABLE DEB (YO)
1   115U 60002D   26122.28646947  .00003555  00000-0  31697-3 0  9991
2   115  48.1632 326.6464 0025720  51.0254 309.2951 14.97940521511252
Epoch: 2026-05-02T06:52Z
TLE epoch observation values (Epoch: 2026-05-02T06:52:30.962Z)
Latitude
0.00004°
Longitude
3.31088°
Altitude
562.313 km
Speed
7.588 km/s
True Right ascension
21h 46m 35s
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
00:44:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
592.207 km
Perigee altitude
556.444 km
Semi-major axis
6,952.462 km
Eccentricity
0.00257
Inclination
48.1632°
RAAN
326.6464°
Arg. of periapsis
51.0254°
True anomaly
309.06655°
Mean anomaly
309.2951°
Eccentric anomaly
309.18087°
Mean motion
3.74399 °/min
Orbital period
96.15 mins
BSTAR
0.00031697
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Other satellites on launch #2 in the year 1960 (1960-04-01 UTC)

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