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
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 19 hours ago

TLE from 19 hours ago
0 THORAD DELTA 1 R/B(2)
1  9330U 74101G   26125.63858626  .00000303  00000-0  10337-2 0  9990
2  9330  13.2254 332.8619 7199573 243.5150  28.3207  2.31240665418067
Epoch: 2026-05-05T15:19Z
TLE epoch observation values (Epoch: 2026-05-05T15:19:33.852Z)
Latitude
-0.00038°
Longitude
-120.62618°
Altitude
10,691.355 km
Speed
5.495 km/s
True Right ascension
22h 11m 06s
True Declination
0° 00' 01"
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
18:06:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,177.888 km
Perigee altitude
387.997 km
Semi-major axis
24,161.079 km
Eccentricity
0.71996
Inclination
13.2254°
RAAN
332.8619°
Arg. of periapsis
243.515°
True anomaly
116.29737°
Mean anomaly
28.3207°
Eccentric anomaly
66.00696°
Mean motion
0.57792 °/min
Orbital period
622.92 mins
BSTAR
0.0010337
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