INTELSAT 33E DEB, 61988
Orbit data source: Space-Track
INTELSAT 33E DEB, 61988 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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61988 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 INTELSAT 33E DEB
1 61988U 16053E 25361.70149936 -.00000266 00000-0 00000-0 0 9998
2 61988 1.2916 98.6860 0055585 132.7226 226.8975 0.99838817 4322Epoch: 2025-12-27T16:50Z
TLE epoch observation values (Epoch: 2025-12-27T16:50:09.544Z)
Latitude
0°
Longitude
108.87462°
Altitude
36,069.965 km
Speed
3.059 km/s
True Right ascension
06h 31m 21s
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
13:59:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,144.532 km
Perigee altitude
35,674.421 km
Semi-major axis
42,287.614 km
Eccentricity
0.00556
Inclination
1.2916°
RAAN
98.686°
Arg. of periapsis
132.7226°
True anomaly
226.43464°
Mean anomaly
226.8975°
Eccentric anomaly
226.66585°
Mean motion
0.24959 °/min
Orbital period
1,442.38 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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61988 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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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 descending order |
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