INTELSAT 33E DEB, 61997
Orbit data source: Space-Track
INTELSAT 33E DEB, 61997 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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61997 intel report (Beta)
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Edit Public Description
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TLE from 2 days ago
0 INTELSAT 33E DEB
1 61997U 16053P 25198.37818144 -.00000213 00000-0 00000-0 0 9995
2 61997 0.7137 92.8654 0090524 258.0458 8.9183 1.01612068 2767
Epoch: 2025-07-17T09:04Z
TLE epoch observation values (Epoch: 2025-07-17T09:04:34.876Z)
Latitude
-0.72675°
Longitude
-71.59032°
Altitude
35,041.731 km
Speed
3.116 km/s
True Right ascension
23h 59m 59s
True Declination
0° 43' 34"
Sunlit
Visualization orbit readout
Latitude
0.5514°
Longitude
151.08623°
Altitude
35,645.249 km
Speed
3.071 km/s
Apparent Right ascension
15h 09m 36s
Apparent Declination
-5° 27' 10"
Sunlit
Visualization observer readout
Local Sidereal Time
12:09:43
Azimuth
126.719° SE
Elevation
28.632°
Doppler factor
1
Orbital elements
Apogee altitude
35,794.418 km
Perigee altitude
35,037.742 km
Semi-major axis
41,794.217 km
Eccentricity
0.00905
Inclination
0.7137°
RAAN
92.8654°
Arg. of periapsis
258.0458°
True anomaly
9.08093°
Mean anomaly
8.9183°
Eccentric anomaly
8.99943°
Mean motion
0.25402 °/min
Orbital period
1,417.21 mins
BSTAR
0
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Other satellites on launch #53 in the year 2016 (2016-08-24 UTC)
INTELSAT 33E DEB Visibility forecast
Observer location: undefined°, undefined°
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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1440 mins | 2025-07-18 23:22:07.568Z | 126.733° SE | 2025-07-18 23:22:07.568Z | 126.733° SE | 25.595° | 2025-07-19 23:22:07.568Z | 122.275° SE |
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61997 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
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