THORAD AGENA D DEB, 9668 (Decayed)
Orbit data source: Space-Track
THORAD AGENA D DEB, 9668 was space debris in SSO originally from a launch on Wed, 08 Apr 1970 UTC launched from the Air Force Western Test Range (AFWTR). 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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9668 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Unknown
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 THORAD AGENA D DEB
1 9668U 70025NM 26052.89495377 .05868375 10242-0 13187-1 0 9992
2 9668 100.0549 26.1605 0019207 162.4336 197.7604 16.04660282565683Epoch: 2026-02-21T21:28Z
TLE epoch observation values (Epoch: 2026-02-21T21:28:44.005Z)
Latitude
-0.00004°
Longitude
-87.83383°
Altitude
276.794 km
Speed
7.734 km/s
True Right ascension
01h 44m 38s
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
15:54:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
271.271 km
Perigee altitude
245.777 km
Semi-major axis
6,636.661 km
Eccentricity
0.00192
Inclination
100.0549°
RAAN
26.1605°
Arg. of periapsis
162.4336°
True anomaly
197.69342°
Mean anomaly
197.7604°
Eccentric anomaly
197.72689°
Mean motion
4.01438 °/min
Orbital period
89.68 mins
BSTAR
0.013187
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Other satellites on launch #25 in the year 1970 (1970-04-08 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.THORAD AGENA D DEB Visibility
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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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| This satellite is decayed. |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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