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

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago
0 THOR ABLE DEB (YO)
1 00115U 60002D   25243.57653131  .00006043  00000-0  55555-3 0  9993
2 00115  48.1622  83.1686 0026805  34.1934 326.0703 14.95592798474745
Epoch: 2025-08-31T13:50Z
TLE epoch observation values (Epoch: 2025-08-31T13:50:12.305Z)
Latitude
-0.00003°
Longitude
-104.37719°
Altitude
565.42 km
Speed
7.588 km/s
True Right ascension
05h 32m 40s
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
12:01:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
600.253 km
Perigee altitude
562.942 km
Semi-major axis
6,959.734 km
Eccentricity
0.00268
Inclination
48.1622°
RAAN
83.1686°
Arg. of periapsis
34.1934°
True anomaly
325.89837°
Mean anomaly
326.0703°
Eccentric anomaly
325.98438°
Mean motion
3.73813 °/min
Orbital period
96.3 mins
BSTAR
0.00055555
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Other satellites on launch #2 in the year 1960 (1960-04-01 UTC)

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