IRIDIUM 33 DEB, 34366

Orbit data source: Space-Track

IRIDIUM 33 DEB, 34366 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
34366, 1997-051FJ
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1997-09-14 (28 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: 13 hours ago

TLE from 13 hours ago
0 IRIDIUM 33 DEB
1 34366U 97051FJ  25348.68584878  .00003618  00000-0  84939-3 0  9994
2 34366  86.3699  48.4671 0022595 133.4897 356.0007 14.54079263882104
Epoch: 2025-12-14T16:27Z
TLE epoch observation values (Epoch: 2025-12-14T16:27:37.334Z)
Latitude
50.48798°
Longitude
-106.42194°
Altitude
704.544 km
Speed
7.517 km/s
True Right ascension
14h 56m 18s
True Declination
50° 19' 04"
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
04:15:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
725.307 km
Perigee altitude
693.279 km
Semi-major axis
7,087.43 km
Eccentricity
0.00226
Inclination
86.3699°
RAAN
48.4671°
Arg. of periapsis
133.4897°
True anomaly
355.98259°
Mean anomaly
356.0007°
Eccentric anomaly
355.99165°
Mean motion
3.63756 °/min
Orbital period
98.97 mins
BSTAR
0.00084939
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|