INTELSAT 33E DEB, 64396
Orbit data source: Space-Track
INTELSAT 33E DEB, 64396 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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64396 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
2 days ago
Origin
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 2 days ago
0 INTELSAT 33E DEB
1 64396U 16053AA 25230.96347615 .00000007 00000-0 00000-0 0 9993
2 64396 0.7790 85.6159 0125410 52.6964 222.6414 0.98612910 3002Epoch: 2025-08-18T23:07Z
TLE epoch observation values (Epoch: 2025-08-18T23:07:24.339Z)
Latitude
-0.7985°
Longitude
45.58644°
Altitude
36,655.919 km
Speed
3.029 km/s
True Right ascension
00h 00m 00s
True Declination
0° 47' 52"
Sunlit
Visualization orbit readout
Latitude
0.17291°
Longitude
-60.57981°
Altitude
36,482.864 km
Speed
3.042 km/s
Apparent Right ascension
17h 09m 52s
Apparent Declination
-4° 48' 32"
Sunlit
Visualization observer readout
Local Sidereal Time
07:24:32
Azimuth
49.737° ENE
Elevation
-43.621°
Doppler factor
1
Orbital elements
Apogee altitude
36,793.919 km
Perigee altitude
35,724.489 km
Semi-major axis
42,637.341 km
Eccentricity
0.01254
Inclination
0.779°
RAAN
85.6159°
Arg. of periapsis
52.6964°
True anomaly
221.67905°
Mean anomaly
222.6414°
Eccentric anomaly
222.15912°
Mean motion
0.24652 °/min
Orbital period
1,460.31 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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64396 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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