DECAYED

IRIDIUM 33 DEB, 34503 (Decayed)

Orbit data source: Space-Track

IRIDIUM 33 DEB, 34503 was 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.

Not visible in the next 10 days
Identifier
34503, 1997-051GU
Orbit
Decayed
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Decayed 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: 9 months ago

TLE from 9 months ago
0 IRIDIUM 33 DEB
1 34503U 97051GU  25089.29461845  .06940213  15778+0  17922-1 0  9994
2 34503  86.2693  28.8465 0018137 176.2823 183.8603 16.03179537856384
Epoch: 2025-03-30T07:04Z
TLE epoch observation values (Epoch: 2025-03-30T07:04:15.034Z)
Latitude
-0.00004°
Longitude
94.85693°
Altitude
280.93 km
Speed
7.732 km/s
True Right ascension
01h 55m 23s
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
02:55:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
274.397 km
Perigee altitude
250.309 km
Semi-major axis
6,640.49 km
Eccentricity
0.00181
Inclination
86.2693°
RAAN
28.8465°
Arg. of periapsis
176.2823°
True anomaly
183.84634°
Mean anomaly
183.8603°
Eccentric anomaly
183.85332°
Mean motion
4.01091 °/min
Orbital period
89.76 mins
BSTAR
0.017922
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|