THORAD AGENA D DEB, 5957 (Decayed)
Orbit data source: Space-Track
THORAD AGENA D DEB, 5957 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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5957 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 THORAD AGENA D DEB
1 05957U 70025MN 25323.07345324 .06927204 87162-1 26688-1 0 9999
2 05957 99.5846 81.1784 0021283 324.5387 35.4464 15.92937161142632Epoch: 2025-11-19T01:45Z
TLE epoch observation values (Epoch: 2025-11-19T01:45:46.359Z)
Latitude
-0.00005°
Longitude
-3.61517°
Altitude
285.623 km
Speed
7.743 km/s
True Right ascension
05h 24m 42s
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
11:11:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
305.242 km
Perigee altitude
276.854 km
Semi-major axis
6,669.185 km
Eccentricity
0.00213
Inclination
99.5846°
RAAN
81.1784°
Arg. of periapsis
324.5387°
True anomaly
35.58815°
Mean anomaly
35.4464°
Eccentric anomaly
35.51724°
Mean motion
3.98505 °/min
Orbital period
90.34 mins
BSTAR
0.026688
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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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