INTELSAT 33E DEB, 64403
Orbit data source: Space-Track
INTELSAT 33E DEB, 64403 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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64403 intel report (Beta)
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Edit Public Description
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TLE from 1 day ago
0 INTELSAT 33E DEB
1 64403U 16053AH 25231.56292955 .00000112 00000-0 00000-0 0 9992
2 64403 0.7211 51.4841 0057867 358.6842 310.3227 1.00714030 2918
Epoch: 2025-08-19T13:30Z
TLE epoch observation values (Epoch: 2025-08-19T13:30:37.113Z)
Latitude
-0.58577°
Longitude
-170.80566°
Altitude
35,506.697 km
Speed
3.091 km/s
True Right ascension
00h 00m 00s
True Declination
0° 35' 07"
Sunlit
Visualization orbit readout
Latitude
-0.11268°
Longitude
-126.65884°
Altitude
35,421.716 km
Speed
3.097 km/s
Apparent Right ascension
02h 31m 20s
Apparent Declination
-5° 56' 56"
Sunlit
Visualization observer readout
Local Sidereal Time
07:10:30
Azimuth
252.184° W
Elevation
11.363°
Doppler factor
1
Orbital elements
Apogee altitude
35,907.431 km
Perigee altitude
35,420.859 km
Semi-major axis
42,042.282 km
Eccentricity
0.00579
Inclination
0.7211°
RAAN
51.4841°
Arg. of periapsis
358.6842°
True anomaly
309.81477°
Mean anomaly
310.3227°
Eccentric anomaly
310.06897°
Mean motion
0.25178 °/min
Orbital period
1,429.84 mins
BSTAR
0
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Other satellites on launch #53 in the year 2016 (2016-08-24 UTC)
INTELSAT 33E DEB Visibility forecast
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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1440 mins | 2025-08-20 16:13:58.286Z | 252.169° W | 2025-08-20 23:33:58.286Z | 251.946° W | 12.593° | 2025-08-21 16:13:58.286Z | 251.003° W |
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64403 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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