INTELSAT 33E DEB, 64404
Orbit data source: Space-Track
INTELSAT 33E DEB, 64404 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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64404 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 INTELSAT 33E DEB
1 64404U 16053AJ 26120.62248940 -.00000270 00000-0 00000-0 0 9999
2 64404 1.3121 59.5237 0111901 25.7285 334.5009 0.99880074 5432Epoch: 2026-04-30T14:56Z
TLE epoch observation values (Epoch: 2026-04-30T14:56:23.084Z)
Latitude
-0.00001°
Longitude
-23.46327°
Altitude
35,469.417 km
Speed
3.102 km/s
True Right ascension
03h 56m 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
20:33:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,370.904 km
Perigee altitude
35,424.759 km
Semi-major axis
42,275.969 km
Eccentricity
0.01119
Inclination
1.3121°
RAAN
59.5237°
Arg. of periapsis
25.7285°
True anomaly
333.94183°
Mean anomaly
334.5009°
Eccentric anomaly
334.22208°
Mean motion
0.24969 °/min
Orbital period
1,441.78 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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64404 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 descending 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 descending order |
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