IRIDIUM 33 DEB, 35797
Orbit data source: Space-Track
IRIDIUM 33 DEB, 35797 is space debris in LEO originally from a launch on Sun, 14 Sep 1997 UTC launched from the Tyuratam Missile And Space Complex (TTMTR). The debris from Iridium 33, an American commercial communications satellite, has been tracked extensively since its accidental collision with the defunct Russian satellite Cosmos 2251 in 2009. This event, occurring at high speed in low Earth orbit (LEO), generated thousands of pieces of space debris, significantly increasing the risk of further collisions. The Iridium 33 debris cloud has impacted space traffic management and orbital debris mitigation strategies, making it a subject of ongoing study in space situational awareness.
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35797 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 IRIDIUM 33 DEB
1 35797U 97051SF 25304.85236443 .00016432 00000-0 21049-2 0 9996
2 35797 86.3391 349.1906 0010500 314.8569 45.1799 14.81179807867201TLE epoch observation values (Epoch: 2025-10-31T20:27:24.286Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #51 in the year 1997 (1997-09-14 UTC)
IRIDIUM 33 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-03 13:53:47.433Z | 45.191° ENE | 2025-11-03 13:55:47.433Z | 73.59° E | 14.507° | 2025-11-03 13:57:47.433Z | 103.179° ESE |
| 7 mins | 2025-11-03 15:30:47.433Z | 337.296° NNW | 2025-11-03 15:33:47.433Z | 270.38° WNW | 34.941° | 2025-11-03 15:37:47.433Z | 201.342° SSW |
| 4 mins | 2025-11-04 02:26:47.433Z | 99.77° ESE | 2025-11-04 02:27:47.433Z | 82.265° E | 17.674° | 2025-11-04 02:30:47.433Z | 38.528° NE |
| 6 mins | 2025-11-04 04:02:47.433Z | 226.592° WSW | 2025-11-04 04:04:47.433Z | 269.182° W | 29.239° | 2025-11-04 04:08:47.433Z | 341.993° N |
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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