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 (52 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
SPHERE + CONE, 1.1 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 18 hours ago

TLE from 18 hours ago
0 THORAD DELTA 1 R/B(2)
1  9330U 74101G   26305.88724735  .00000891  00000-0  17275-2 0  9990
2  9330  12.7626 262.8436 7201521  19.4000 357.6843  2.31372054422230
Epoch: 2026-11-01T21:17Z
TLE epoch observation values (Epoch: 2026-11-01T21:17:38.171Z)
Latitude
0.00041°
Longitude
-97.73035°
Altitude
555.737 km
Speed
9.922 km/s
True Right ascension
17h 31m 24s
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
11:23:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,166.923 km
Perigee altitude
380.741 km
Semi-major axis
24,151.969 km
Eccentricity
0.72015
Inclination
12.7626°
RAAN
262.8436°
Arg. of periapsis
19.4°
True anomaly
339.8389°
Mean anomaly
357.6843°
Eccentric anomaly
351.79718°
Mean motion
0.57825 °/min
Orbital period
622.57 mins
BSTAR
0.0017275
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