THOR ABLESTAR R/B, 59

Orbit data source: Space-Track

THOR ABLESTAR R/B, 59 is space debris in LEO originally from a launch on Tue, 04 Oct 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
59, 1960-013B
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Aerojet
Mission
Spacecraft
Bus & Motor
ABLESTAR, Unknown motor
Mass
600 kg wet, 600 kg dry
Launch date (UTC)
1960-10-04 (65 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 2.4 m
Radar Cross Section
6.048 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 21 hours ago

TLE from 21 hours ago
0 THOR ABLESTAR R/B
1 00059U 60013B   25242.10428207  .00000167  00000-0  10805-3 0  9994
2 00059  28.2469 179.2087 0188864  32.0328 329.1544 13.53143944203712
Epoch: 2025-08-30T02:30Z
TLE epoch observation values (Epoch: 2025-08-30T02:30:09.97Z)
Latitude
-0.00005°
Longitude
163.12369°
Altitude
939.209 km
Speed
7.444 km/s
True Right ascension
11h 56m 50s
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
15:33:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,205.221 km
Perigee altitude
924.086 km
Semi-major axis
7,442.79 km
Eccentricity
0.01889
Inclination
28.2469°
RAAN
179.2087°
Arg. of periapsis
32.0328°
True anomaly
328.02188°
Mean anomaly
329.1544°
Eccentric anomaly
328.59046°
Mean motion
3.38018 °/min
Orbital period
106.5 mins
BSTAR
0.00010805
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Other satellites on launch #13 in the year 1960 (1960-10-04 UTC)

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