DODECAPOLE 2 DEB, 41734
Orbit data source: Space-Track
DODECAPOLE 2 DEB, 41734 is space debris in LEO originally from a launch on Fri, 13 Aug 1965 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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41734 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.050 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 DODECAPOLE 2 DEB
1 41734U 65065U 26304.96868878 .00003996 00000-0 17671-2 0 9997
2 41734 90.0460 23.4899 0028990 31.4641 328.8277 14.22873585555762Epoch: 2026-10-31T23:14Z
TLE epoch observation values (Epoch: 2026-10-31T23:14:54.710Z)
Latitude
-0.00005°
Longitude
-5.50486°
Altitude
800.879 km
Speed
7.462 km/s
True Right ascension
01h 33m 57s
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
07:21:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
833.441 km
Perigee altitude
791.749 km
Semi-major axis
7,190.732 km
Eccentricity
0.0029
Inclination
90.046°
RAAN
23.4899°
Arg. of periapsis
31.4641°
True anomaly
328.65521°
Mean anomaly
328.8277°
Eccentric anomaly
328.74151°
Mean motion
3.55945 °/min
Orbital period
101.14 mins
BSTAR
0.0017671
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Other satellites on launch #65 in the year 1965 (1965-08-13 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.DODECAPOLE 2 DEB Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-11-01 16:42:36.418Z | 31.38° NE | 2026-11-01 16:46:36.418Z | 80.759° E | 23.544° | 2026-11-01 16:50:36.418Z | 132.313° SE |
| 8 mins | 2026-11-01 18:24:36.418Z | 337.614° N | 2026-11-01 18:27:36.418Z | 287.482° WNW | 40.178° | 2026-11-01 18:32:36.418Z | 212.431° SW |
| 10 mins | 2026-11-02 05:43:36.418Z | 176.579° S | 2026-11-02 05:48:36.418Z | 185.194° SSW | 82.638° | 2026-11-02 05:53:36.418Z | 357.427° N |
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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