INTELSAT 33E DEB, 64408
Orbit data source: Space-Track
INTELSAT 33E DEB, 64408 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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64408 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
1 day ago
Origin
INTELU (Unknown / ITSO)Manufacturer
Boeing/ES
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & history
TLE from 1 day ago
0 INTELSAT 33E DEB
1 64408U 16053AN 25231.26834407 -.00000126 00000-0 00000-0 0 9994
2 64408 1.5356 97.4314 1022883 342.7088 14.1393 1.03191913 2964Epoch: 2025-08-19T06:26Z
TLE epoch observation values (Epoch: 2025-08-19T06:26:24.927Z)
Latitude
0.00001°
Longitude
33.03174°
Altitude
30,918.839 km
Speed
3.426 km/s
True Right ascension
06h 29m 59s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
0.51791°
Longitude
-166.22128°
Altitude
39,202.149 km
Speed
2.803 km/s
Apparent Right ascension
17h 24m 09s
Apparent Declination
-4° 11' 42"
Sunlit
Visualization observer readout
Local Sidereal Time
07:12:01
Azimuth
41.329° NE
Elevation
-46.778°
Doppler factor
1
Orbital elements
Apogee altitude
39,219.766 km
Perigee altitude
30,757.131 km
Semi-major axis
41,366.586 km
Eccentricity
0.10229
Inclination
1.5356°
RAAN
97.4314°
Arg. of periapsis
342.7088°
True anomaly
17.40338°
Mean anomaly
14.1393°
Eccentric anomaly
15.72796°
Mean motion
0.25797 °/min
Orbital period
1,395.51 mins
BSTAR
0
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Other satellites on launch #53 in the year 2016 (2016-08-24 UTC)
INTELSAT 33E DEB Visibility
Observer location: undefined°, undefined°
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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64408 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
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