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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9330 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast 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
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
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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Other satellites on launch #101 in the year 1974 (1974-12-19 UTC)
THORAD DELTA 1 R/B(2) Visibility forecast
Observer location: undefined°, undefined°
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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451 mins | 2025-09-01 00:44:23.273Z | 232.192° WSW | 2025-09-01 01:46:23.273Z | 178.449° S | 29.606° | 2025-09-01 08:15:23.273Z | 211.475° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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