INTELSAT 33E DEB, 61991
Orbit data source: Space-Track
INTELSAT 33E DEB, 61991 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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61991 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 INTELSAT 33E DEB
1 61991U 16053H 26120.59544392 .00000032 00000-0 00000-0 0 9998
2 61991 1.5475 92.7909 0120867 255.9213 102.9917 1.02041491 5700Epoch: 2026-04-30T14:17Z
TLE epoch observation values (Epoch: 2026-04-30T14:17:26.354Z)
Latitude
-0°
Longitude
20.14789°
Altitude
35,413.455 km
Speed
3.084 km/s
True Right ascension
06h 12m 11s
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
23:06:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,802.484 km
Perigee altitude
34,795.012 km
Semi-major axis
41,676.885 km
Eccentricity
0.01209
Inclination
1.5475°
RAAN
92.7909°
Arg. of periapsis
255.9213°
True anomaly
104.33659°
Mean anomaly
102.9917°
Eccentric anomaly
103.66462°
Mean motion
0.25509 °/min
Orbital period
1,411.24 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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61991 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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