IRIDIUM 33 DEB, 34497

Orbit data source: Space-Track

IRIDIUM 33 DEB, 34497 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
34497, 1997-051GN
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: 2 days ago

TLE from 2 days ago
0 IRIDIUM 33 DEB
1 34497U 97051GN  26087.22302490  .00002078  00000-0  80484-3 0  9998
2 34497  86.2831   7.3279 0080190   0.0866 152.3883 14.27864199883889
Epoch: 2026-03-28T05:21Z
TLE epoch observation values (Epoch: 2026-03-28T05:21:09.351Z)
Latitude
27.0779°
Longitude
-80.50064°
Altitude
853.412 km
Speed
7.402 km/s
True Right ascension
12h 21m 44s
True Declination
26° 56' 26"
Sunlit
Object was in full shadow 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
00:06:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
853.383 km
Perigee altitude
738.326 km
Semi-major axis
7,173.991 km
Eccentricity
0.00802
Inclination
86.2831°
RAAN
7.3279°
Arg. of periapsis
0.0866°
True anomaly
152.81044°
Mean anomaly
152.3883°
Eccentric anomaly
152.59974°
Mean motion
3.57192 °/min
Orbital period
100.79 mins
BSTAR
0.00080484
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|