IRIDIUM 33 DEB, 36080
Orbit data source: Space-Track
IRIDIUM 33 DEB, 36080 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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36080 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.050 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 4 days ago
TLE from 4 days ago
0 IRIDIUM 33 DEB
1 36080U 97051VM 26310.50277672 .00001640 00000-0 43823-3 0 9991
2 36080 86.3220 224.5782 0017702 143.4383 216.8032 14.47716926521695Epoch: 2026-11-06T12:03Z
TLE epoch observation values (Epoch: 2026-11-06T12:03:59.908Z)
Latitude
-0.00008°
Longitude
-2.14288°
Altitude
746.274 km
Speed
7.476 km/s
True Right ascension
14h 58m 18s
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
22:25:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
742.645 km
Perigee altitude
717.479 km
Semi-major axis
7,108.199 km
Eccentricity
0.00177
Inclination
86.322°
RAAN
224.5782°
Arg. of periapsis
143.4383°
True anomaly
216.68189°
Mean anomaly
216.8032°
Eccentric anomaly
216.74253°
Mean motion
3.62163 °/min
Orbital period
99.4 mins
BSTAR
0.00043823
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Other satellites on launch #51 in the year 1997 (1997-09-14 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.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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-11-10 06:12:57.108Z | 0.098° NNE | 2026-11-10 06:16:57.108Z | 37.271° NE | 75.692° | 2026-11-10 06:21:57.108Z | 174.983° S |
| 4 mins | 2026-11-10 17:24:57.108Z | 102.32° ESE | 2026-11-10 17:26:57.108Z | 75.494° E | 15.3° | 2026-11-10 17:28:57.108Z | 50.049° ENE |
| 7 mins | 2026-11-10 19:02:57.108Z | 205.984° SW | 2026-11-10 19:05:57.108Z | 274.53° WNW | 53.791° | 2026-11-10 19:09:57.108Z | 349.866° 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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