THORAD AGENA D DEB, 42493 (Decayed)
Orbit data source: Space-Track
THORAD AGENA D DEB, 42493 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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42493 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 THORAD AGENA D DEB
1 42493U 70025QX 24178.37621620 .00070292 00000-0 60088-2 0 9999
2 42493 99.4603 8.5287 0007605 349.5958 131.2546 14.97280019560572
Epoch: 2024-06-26T09:01Z
TLE epoch observation values (Epoch: 2024-06-26T09:01:45.079Z)
Latitude
57.9096°
Longitude
153.43214°
Altitude
588.515 km
Speed
7.57 km/s
True Right ascension
13h 35m 24s
True Declination
57° 45' 03"
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
12:20:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
577.686 km
Perigee altitude
567.114 km
Semi-major axis
6,950.537 km
Eccentricity
0.00076
Inclination
99.4603°
RAAN
8.5287°
Arg. of periapsis
349.5958°
True anomaly
131.32007°
Mean anomaly
131.2546°
Eccentric anomaly
131.28734°
Mean motion
3.74555 °/min
Orbital period
96.11 mins
BSTAR
0.0060088
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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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