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
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 22 hours ago

TLE from 22 hours ago
0 THOR ABLESTAR R/B
1 00059U 60013B   26057.99896331  .00000154  00000-0  89034-4 0  9990
2 00059  28.2491 329.7179 0188979 110.7631 251.3270 13.53162996228233
Epoch: 2026-02-26T23:58Z
TLE epoch observation values (Epoch: 2026-02-26T23:58:30.429Z)
Latitude
-0.00005°
Longitude
173.24928°
Altitude
1,106.373 km
Speed
7.278 km/s
True Right ascension
21h 58m 52s
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
01:03:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,205.235 km
Perigee altitude
923.931 km
Semi-major axis
7,442.72 km
Eccentricity
0.0189
Inclination
28.2491°
RAAN
329.7179°
Arg. of periapsis
110.7631°
True anomaly
249.29128°
Mean anomaly
251.327°
Eccentric anomaly
250.30756°
Mean motion
3.38023 °/min
Orbital period
106.5 mins
BSTAR
0.000089034
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Other satellites on launch #13 in the year 1960 (1960-10-04 UTC)

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