IRIDIUM 33 DEB, 38241

Orbit data source: Space-Track

IRIDIUM 33 DEB, 38241 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.

Loading next visibility...
Identifier
38241, 1997-051ZR
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1997-09-14 (29 years ago)
Launch vehicle
Unknown
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago
0 IRIDIUM 33 DEB
1 38241U 97051ZR  26085.32979819  .00002323  00000-0  52754-3 0  9995
2 38241  86.3192 304.8842 0005163  73.7034 286.4741 14.55641502617073
Epoch: 2026-03-26T07:54Z
TLE epoch observation values (Epoch: 2026-03-26T07:54:54.563Z)
Latitude
-0.00004°
Longitude
2.37655°
Altitude
709.327 km
Speed
7.502 km/s
True Right ascension
20h 19m 32s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
23:35:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
707.875 km
Perigee altitude
700.562 km
Semi-major axis
7,082.355 km
Eccentricity
0.00052
Inclination
86.3192°
RAAN
304.8842°
Arg. of periapsis
73.7034°
True anomaly
286.41735°
Mean anomaly
286.4741°
Eccentric anomaly
286.44573°
Mean motion
3.64147 °/min
Orbital period
98.86 mins
BSTAR
0.00052754
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|