THORAD AGENA D DEB, 42507 (Decayed)
Orbit data source: Space-Track
THORAD AGENA D DEB, 42507 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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42507 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 6 months ago
TLE from 6 months ago
0 THORAD AGENA D DEB
1 42507U 70025RM 25106.81345943 .00104265 00000-0 99467-2 0 9998
2 42507 99.1801 306.3879 0020656 230.2037 129.7360 14.92623588581448
Epoch: 2025-04-16T19:31Z
TLE epoch observation values (Epoch: 2025-04-16T19:31:22.894Z)
Latitude
0.00001°
Longitude
168.34818°
Altitude
601.976 km
Speed
7.554 km/s
True Right ascension
20h 25m 33s
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
15:19:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
601.232 km
Perigee altitude
572.458 km
Semi-major axis
6,964.982 km
Eccentricity
0.00207
Inclination
99.1801°
RAAN
306.3879°
Arg. of periapsis
230.2037°
True anomaly
129.91772°
Mean anomaly
129.736°
Eccentric anomaly
129.82689°
Mean motion
3.7339 °/min
Orbital period
96.41 mins
BSTAR
0.0099467
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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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