INTELSAT 33E DEB, 64402
Orbit data source: Space-Track
INTELSAT 33E DEB, 64402 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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64402 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 INTELSAT 33E DEB
1 64402U 16053AG 26120.13478448 -.00000278 00000-0 00000-0 0 9999
2 64402 1.3885 75.3648 0122264 101.2162 260.1888 0.98357244 5398Epoch: 2026-04-30T03:14Z
TLE epoch observation values (Epoch: 2026-04-30T03:14:05.379Z)
Latitude
-0.00001°
Longitude
168.78405°
Altitude
36,429.532 km
Speed
3.048 km/s
True Right ascension
05h 01m 34s
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
21:43:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,855.258 km
Perigee altitude
35,810.85 km
Semi-major axis
42,711.191 km
Eccentricity
0.01223
Inclination
1.3885°
RAAN
75.3648°
Arg. of periapsis
101.2162°
True anomaly
258.81197°
Mean anomaly
260.1888°
Eccentric anomaly
259.50001°
Mean motion
0.24588 °/min
Orbital period
1,464.1 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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64402 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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