THORAD DELTA 1 R/B(2), 9330

Orbit data source: Space-Track

THORAD DELTA 1 R/B(2), 9330 is space debris in HEO originally from a launch on Thu, 19 Dec 1974 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
9330, 1974-101G
Orbit
HEO
Country
Flag of USUS
Related business
Manufacturer
Thiokol/TE
Mission
Spacecraft
Bus & Motor
STAR 37, Unknown motor
Mass
~83 kg wet, 83 kg dry
Launch date (UTC)
1974-12-19 (51 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Domed Cyl + 1 Nozzle, 0.8 m
Radar Cross Section
1.559 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 THORAD DELTA 1 R/B(2)
1 09330U 74101G   25242.27437840  .00000654  00000-0  20510-2 0  9993
2 09330  13.0418  70.1814 7196369  55.6983 352.9220  2.31078188412314
Epoch: 2025-08-30T06:35Z
TLE epoch observation values (Epoch: 2025-08-30T06:35:06.293Z)
Latitude
-0.00013°
Longitude
-7.20412°
Altitude
1,896.018 km
Speed
8.936 km/s
True Right ascension
04h 41m 07s
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
23:53:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,189.619 km
Perigee altitude
398.913 km
Semi-major axis
24,172.403 km
Eccentricity
0.71964
Inclination
13.0418°
RAAN
70.1814°
Arg. of periapsis
55.6983°
True anomaly
305.37505°
Mean anomaly
352.922°
Eccentric anomaly
336.44331°
Mean motion
0.57752 °/min
Orbital period
623.36 mins
BSTAR
0.002051
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