IRIDIUM 33 DEB, 38228
Orbit data source: Space-Track
IRIDIUM 33 DEB, 38228 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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38228 intel report (Beta)
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Edit Public Description
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, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 IRIDIUM 33 DEB
1 38228U 97051ZC 25303.12017250 .00001243 00000-0 49184-3 0 9995
2 38228 86.2938 67.0073 0063247 333.1222 209.6749 14.27133144841596Epoch: 2025-10-30T02:53Z
TLE epoch observation values (Epoch: 2025-10-30T02:53:02.903Z)
Latitude
-2.56984°
Longitude
165.22737°
Altitude
844.27 km
Speed
7.41 km/s
True Right ascension
16h 28m 41s
True Declination
-2° 33' 17"
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
03:02:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
843.695 km
Perigee altitude
752.917 km
Semi-major axis
7,176.443 km
Eccentricity
0.00632
Inclination
86.2938°
RAAN
67.0073°
Arg. of periapsis
333.1222°
True anomaly
209.31854°
Mean anomaly
209.6749°
Eccentric anomaly
209.49648°
Mean motion
3.57009 °/min
Orbital period
100.84 mins
BSTAR
0.00049184
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-11-01 08:00:03.456Z | 138.292° SSE | 2025-11-01 08:04:03.456Z | 77.914° E | 26.521° | 2025-11-01 08:08:03.456Z | 25.709° NE |
| 7 mins | 2025-11-01 09:42:03.456Z | 233.13° WSW | 2025-11-01 09:45:03.456Z | 282.764° WNW | 26.112° | 2025-11-01 09:49:03.456Z | 337.711° N |
| 9 mins | 2025-11-01 20:15:03.456Z | 2.792° NNE | 2025-11-01 20:19:03.456Z | 133.94° SE | 43.71° | 2025-11-01 20:24:03.456Z | 173.807° S |
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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