INTELSAT 33E DEB, 64405
Orbit data source: Space-Track
INTELSAT 33E DEB, 64405 is space debris in GEO originally from a launch on Wed, 24 Aug 2016 UTC launched from the French Guiana (FRGUI). 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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64405 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 INTELSAT 33E DEB
1 64405U 16053AK 25291.84394936 -.00000326 00000-0 00000-0 0 9991
2 64405 1.1053 101.1707 0074844 17.9342 343.5299 0.99506652 3506
Epoch: 2025-10-18T20:15Z
TLE epoch observation values (Epoch: 2025-10-18T20:15:17.224Z)
Latitude
-0°
Longitude
130.97434°
Altitude
35,699.686 km
Speed
3.089 km/s
True Right ascension
06h 49m 27s
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
05:56:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,320.729 km
Perigee altitude
35,686.326 km
Semi-major axis
42,381.664 km
Eccentricity
0.00748
Inclination
1.1053°
RAAN
101.1707°
Arg. of periapsis
17.9342°
True anomaly
343.28454°
Mean anomaly
343.5299°
Eccentric anomaly
343.40744°
Mean motion
0.24876 °/min
Orbital period
1,447.19 mins
BSTAR
0
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Other satellites on launch #53 in the year 2016 (2016-08-24 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.INTELSAT 33E 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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INTELSAT 33E DEB is likely not visible in the next few days. |
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64405 neighbors
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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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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