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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Edit Public Description
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, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 DODECAPOLE 2 DEB
1 41734U 65065U 26020.25123611 .00014417 00000-0 67535-2 0 9997
2 41734 90.0440 22.0466 0028620 233.1726 126.6839 14.19895162515316Epoch: 2026-01-20T06:01Z
TLE epoch observation values (Epoch: 2026-01-20T06:01:46.799Z)
Latitude
-0.00002°
Longitude
171.96582°
Altitude
841.119 km
Speed
7.426 km/s
True Right ascension
01h 28m 11s
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
22:11:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
843.265 km
Perigee altitude
802.047 km
Semi-major axis
7,200.793 km
Eccentricity
0.00286
Inclination
90.044°
RAAN
22.0466°
Arg. of periapsis
233.1726°
True anomaly
126.94634°
Mean anomaly
126.6839°
Eccentric anomaly
126.81518°
Mean motion
3.552 °/min
Orbital period
101.35 mins
BSTAR
0.0067535
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-01-20 23:05:20.342Z | 111.74° ESE | 2026-01-20 23:08:20.342Z | 77.035° E | 17.025° | 2026-01-20 23:11:20.342Z | 40.321° NE |
| 9 mins | 2026-01-21 00:45:20.342Z | 196.608° SSW | 2026-01-21 00:49:20.342Z | 272.124° WNW | 39.903° | 2026-01-21 00:54:20.342Z | 348.116° N |
| 7 mins | 2026-01-21 11:23:20.342Z | 38.34° NE | 2026-01-21 11:26:20.342Z | 81.478° E | 23.655° | 2026-01-21 11:30:20.342Z | 135.45° SSE |
| 8 mins | 2026-01-21 13:04:20.342Z | 336.222° NNW | 2026-01-21 13:07:20.342Z | 290.478° WNW | 30.368° | 2026-01-21 13:12:20.342Z | 216.459° SW |
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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