INTELSAT 33E DEB, 61990
Orbit data source: Space-Track
INTELSAT 33E DEB, 61990 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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61990 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / ITSORelated business
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 & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 INTELSAT 33E DEB
1 61990U 16053G 25258.19437524 -.00000336 00000-0 00000-0 0 9990
2 61990 0.7742 71.5715 0104326 341.0825 308.2908 1.01384490 3364Epoch: 2025-09-15T04:39Z
TLE epoch observation values (Epoch: 2025-09-15T04:39:54.02Z)
Latitude
-0.74164°
Longitude
-64.37616°
Altitude
35,208.962 km
Speed
3.106 km/s
True Right ascension
00h 00m 00s
True Declination
0° 44' 27"
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
14:11:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,915.272 km
Perigee altitude
35,041.923 km
Semi-major axis
41,856.735 km
Eccentricity
0.01043
Inclination
0.7742°
RAAN
71.5715°
Arg. of periapsis
341.0825°
True anomaly
307.34489°
Mean anomaly
308.2908°
Eccentric anomaly
307.81861°
Mean motion
0.25345 °/min
Orbital period
1,420.39 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 forecast
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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. |
|---|---|---|---|---|---|---|---|
| 1440 mins | 2025-09-15 21:31:21.658Z | 123.626° SE | 2025-09-15 21:31:21.658Z | 123.626° SE | 23.391° | 2025-09-16 21:31:21.658Z | 120.165° SE |
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61990 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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