THORAD AGENA D DEB, 4190 (Decayed)
Orbit data source: Space-Track
THORAD AGENA D DEB, 4190 was space debris in LEO originally from a launch on Tue, 30 Sep 1969 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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4190 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 year ago
TLE from 1 year ago
0 THORAD AGENA D DEB
1 04190U 69082BD 25052.33546809 .17677494 43718-5 21895-2 0 9991
2 04190 69.9747 346.9478 0009344 201.4829 158.6009 16.35790429919740Epoch: 2025-02-21T08:03Z
TLE epoch observation values (Epoch: 2025-02-21T08:03:04.442Z)
Latitude
-0.00007°
Longitude
74.68103°
Altitude
185.297 km
Speed
7.792 km/s
True Right ascension
23h 07m 47s
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
16:22:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
180.975 km
Perigee altitude
168.728 km
Semi-major axis
6,552.989 km
Eccentricity
0.00093
Inclination
69.9747°
RAAN
346.9478°
Arg. of periapsis
201.4829°
True anomaly
158.63992°
Mean anomaly
158.6009°
Eccentric anomaly
158.62042°
Mean motion
4.09151 °/min
Orbital period
87.99 mins
BSTAR
0.0021895
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Other satellites on launch #82 in the year 1969 (1969-09-30 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
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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