IRIDIUM 33 DEB, 34079

Orbit data source: Space-Track

IRIDIUM 33 DEB, 34079 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
34079, 1997-051CN
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, 0.2 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 IRIDIUM 33 DEB
1 34079U 97051CN  26139.42305175  .00007471  00000-0  79558-3 0  9999
2 34079  86.3725 296.5974 0008165 135.9428 253.3791 14.88769465913203
Epoch: 2026-05-19T10:09Z
TLE epoch observation values (Epoch: 2026-05-19T10:09:11.671Z)
Latitude
29.2161°
Longitude
-90.77764°
Altitude
607.228 km
Speed
7.557 km/s
True Right ascension
19h 54m 28s
True Declination
29° 04' 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
03:52:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
604.364 km
Perigee altitude
592.971 km
Semi-major axis
6,976.804 km
Eccentricity
0.00082
Inclination
86.3725°
RAAN
296.5974°
Arg. of periapsis
135.9428°
True anomaly
253.28947°
Mean anomaly
253.3791°
Eccentric anomaly
253.33428°
Mean motion
3.72442 °/min
Orbital period
96.66 mins
BSTAR
0.00079558
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|