INTELSAT 33E DEB, 61995
Orbit data source: Space-Track
INTELSAT 33E DEB, 61995 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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61995 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 shape, 1.1 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 INTELSAT 33E DEB
1 61995U 16053M 26030.12178769 -.00000252 00000-0 00000-0 0 9997
2 61995 1.1894 84.4678 0053726 278.6046 80.4661 1.01041317 4735Epoch: 2026-01-30T02:55Z
TLE epoch observation values (Epoch: 2026-01-30T02:55:22.456Z)
Latitude
0°
Longitude
-89.03322°
Altitude
35,536.853 km
Speed
3.085 km/s
True Right ascension
05h 36m 42s
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
05:34:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,798.701 km
Perigee altitude
35,347.924 km
Semi-major axis
41,951.449 km
Eccentricity
0.00537
Inclination
1.1894°
RAAN
84.4678°
Arg. of periapsis
278.6046°
True anomaly
81.07392°
Mean anomaly
80.4661°
Eccentric anomaly
80.76994°
Mean motion
0.25259 °/min
Orbital period
1,425.21 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 | 2026-01-31 03:53:33.256Z | 151.614° SSE | 2026-01-31 08:55:33.256Z | 151.125° SSE | 33.312° | 2026-02-01 03:53:33.256Z | 147.878° SSE |
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61995 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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