INTELSAT 33E DEB, 64398
Orbit data source: Space-Track
INTELSAT 33E DEB, 64398 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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64398 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
21 hours 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 21 hours ago
0 INTELSAT 33E DEB
1 64398U 16053AC 25231.79733343 -.00000360 00000-0 00000-0 0 9997
2 64398 0.8436 30.1806 0073386 0.1363 330.0870 1.00970625 2969Epoch: 2025-08-19T19:08Z
TLE epoch observation values (Epoch: 2025-08-19T19:08:09.608Z)
Latitude
-0.44568°
Longitude
104.57835°
Altitude
35,325.383 km
Speed
3.101 km/s
True Right ascension
00h 00m 00s
True Declination
0° 26' 43"
Sunlit
Visualization orbit readout
Latitude
-0.79958°
Longitude
66.34803°
Altitude
35,476.371 km
Speed
3.09 km/s
Apparent Right ascension
21h 14m 19s
Apparent Declination
-5° 45' 56"
Sunlit
Visualization observer readout
Local Sidereal Time
07:20:49
Azimuth
315.703° NNW
Elevation
-47.38°
Doppler factor
1
Orbital elements
Apogee altitude
35,900.899 km
Perigee altitude
35,284.882 km
Semi-major axis
41,971.027 km
Eccentricity
0.00734
Inclination
0.8436°
RAAN
30.1806°
Arg. of periapsis
0.1363°
True anomaly
329.66428°
Mean anomaly
330.087°
Eccentric anomaly
329.87598°
Mean motion
0.25242 °/min
Orbital period
1,426.21 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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64398 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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