INTELSAT 33E DEB, 61994
Orbit data source: Space-Track
INTELSAT 33E DEB, 61994 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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61994 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 INTELSAT 33E DEB
1 61994U 16053L 25321.00491638 .00000169 00000-0 00000-0 0 9994
2 61994 1.0367 89.1918 0025533 204.0506 155.5966 1.00506857 3966Epoch: 2025-11-17T00:07Z
TLE epoch observation values (Epoch: 2025-11-17T00:07:04.775Z)
Latitude
-0.00001°
Longitude
30.84982°
Altitude
35,818.08 km
Speed
3.07 km/s
True Right ascension
05h 55m 43s
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
08:35:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,829.39 km
Perigee altitude
35,614.402 km
Semi-major axis
42,100.033 km
Eccentricity
0.00255
Inclination
1.0367°
RAAN
89.1918°
Arg. of periapsis
204.0506°
True anomaly
155.71713°
Mean anomaly
155.5966°
Eccentric anomaly
155.6569°
Mean motion
0.25126 °/min
Orbital period
1,432.79 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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61994 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 ascending 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 ascending order |
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